MGT File Quick Reference

*COMMAND (Functions of midas)

Brief descriptions of the Commands

; Variables that make up the Commands

Description of each variable (method of expression) {initialized value}

* X,Y,Z axis: Basis of Global coordinates

x,y,z axis: Basis of nodal or element local coordinates

*VERSION

Shows the version of MIDAS/Gen

*UNIT (Unit System)

; FORCE, LENGTH

; FORCE, LENGTH

FORCE: Loading unit used in creating MGT File {tonf}

:LENGTH Length unit used in creating the MGT File {m}

* ENDDATA (End Data)

Completion of Data input

*PROJINFO (Project Information)

Basic project data

PROJECT, REVISION, USER, EMAIL, ADDRESS,

TEL, FAX, CLIENT, TITLE, ENGINEER, EDATE

CHECK1, CDATE1, CHECK2, CDATE2, CHECK3,

CDATE3, APPROVE, ADATE, COMMENT

PROJECT: project name

REVISION: date of final revision

USER: user name

EMAIL: e-mail address

ADDRESS: postal address line

FAX: fax number

CLIENT: client name

TITLE: sub-title of project (sub-project name)

ENGINEER: name of engineer

EDATE: date of program operation

CHECK1: 1st reviewer

CDATE1 : date of 1st review

CHECK2: 2nd reviewer

CDATE2: date of 2nd review

CHECK3: 3nd reviewer

CDATE3: date of 3nd review

APPROVE: final approver

ADATE: date of final approval

COMMENT: notes & comments

*STRUCTYPE (Structure Type)

Basic data required for Structural Analysis

; iSTYP, iSMAS, GRAV, TEMPER, bALIGNBEAM,

bALIGNSLAB

iSTYP: structural type {0}

= 0: 3-dimensional analysis

= 1: 2-dimensional analysis (X-Zplane)

= 2: 2-dimensional analysis (Y-Zplane)

= 3: 2-dimensional analysis (X-Yplane)

= 4: 3-dimensional analysis (restraint on rotational degree of

freedom about Z-direction)

iSMAS: assigns whether to convert the model self-weight to

masses {0}

= 0: does not convert to masses

= 1: converts to masses & applies to X,Y,Z directions in the global

coordinate system

= 2: converts to masses & applies to X,Y directions in the global

coordinate system

= 3: converts to masses & applies to Z direction in the global

coordinate system

GRAV: value of acceleration of gravity considering the applied

units {9.806 m/sec2}

TEMPER: initial temperature required for heat stress analysis

bALIGNBEAM: alligns the tops of girders to Floor Level

(YES/NO) {NO}

bALIGNSLAB: alligns the top of slabs to Floor Level

(YES/NO) {NO}

*GRIDLINE*(Define Line Grid)

Gridline

; NAME, X, Y

NAME: name of gridline

X: X coordinates of GCS (Global Coordinate System) Y-axis

direction and gridlines

Y: Y coordinates of GCS (Global Coordinate System) X-axis

direction and gridlines

*NODE (Nodes)

Node data

; iNO, X, Y, Z

iNO: node number

X: X-coordinate in GCS (Global Coordinate System)

Y: Y-coordinate in GCS (Global Coordinate System)

Z: Z-coordinate in GCS (Global Coordinate System)

*ELEMENT (Elements)

Element Data

; iEL, TYPE, iMAT, iPRO, iN1, iN2, ANGLE,

iSUB, EXVAL                    ; Frame Element

; iEL, TYPE, iMAT, iPRO, iN1, iN2, iN3, iN4

iSUB, iWID                       ; Planar Element

; iEL, TYPE, iMAT, iPRO, iN1, iN2, iN3, iN4,

iN5, iN6, iN7, iN8                 ; Solid Element

1.Frame Element

iEL: element number

TYPE: element type

=TRUSS: truss element

=BEAM: beam element

=TENSTR: tension-only element

=COMPTR: compresion-only element

iMAT: material number

iPRO: section number

iN1: 1st node number

iN2: 2nd node number

ANGLE: Beta Angle

iSUB: Sub Type

For Truss: N/A

For Beam: N/A

For TENSTR & COMPTR {1}

=1: TENSTR-TRUSS, COMPTR-TRUSS

=2: TENSTR-HOOK, COMPTR-GAP

=3: TENSTR-CABLE

EXVAL: additional data related to entered elements

For Truss: N/A

For Beam: N/A

For TENSTR

=TRUSS: N/A

=HOOK: Hook Distance

=Cable: Cable Pretension

For COMPTR

=TRUSS: N/A

=GAP: Gap Diatance

= WALL: wall element

 

2. Planar Element

iEL: element number

TYPE: element type

=PLATE: plate element

=PLSTRS: plane stress element

=PLSTRN: plane strain element

=AXISYM: axis symmetric element

iMAT: material number

iPRO: section number

iN1: 1st node number

iN2: 2nd node numberiN

iN3: 3rd node number

iN4: 4th node number

iSUB: Sub Type

For Plate {1}

=1: Thick   = 2: Thin

For PLSTRS: N/A

For PLSTRN: N/A

For Axisymmetric: N/A

For Wall {1}  

=1: Membrane   

=2: Plate

iWID: wall (combination of elements) ID

 

3.Solid Element

iEL: element number

TYPE : element type

=SOLID: solid element

iMAT: material number

iPRO: section number

iN1: 1st node number

iN2: 2nd node number

iN3: 3rd node number

iN4: 4th node number

iN5: 5th node number

iN6: 6th node number

iN7: 7th node number

iN8: 8th node number

 

4. Frame (Ref. Point)

REF: assign ref. point

RPX: X-coordinate of ref. point

RPZ: Z-coordinate of ref. point

*MATERIAL (Material)

Material property

; iMAT, TYPE, MNAME, SPHEAT, HEATCO, [DATA1]

; STEEL, CONC, USER

; iMAT, TYPE, MNAME, SPHEAT, HEATCO, [DATA1],

[DATA2]                    ; SRC

; [DATA1]: 1, DB, NAME

2, ELAST, POISN, THERMAL, DEN

3, Ex, Ey, Ez, Tx, Ty, Tz, Sxy, Sxz, Syz, Pxy, Pxz,

Pyz, DEN : Orthotropic

; [DATA2]: 1, DB, NAME or 2, ELAST, POISN, THERMAL

DEN

iMAT: material number

TYPE: material type

=STEEL (structural steel)

=CONC (concrete)

=SRC(steel-concrete composite)

=USER(user defined)

MNAME: material name

SPHEAT: specific heat

HEATCO: thermal conductivity coefficient

[DATA 1]

DB: section database of various national standards

NAME: name of DB

[DATA 2]

ELAST: modulus of elasticity

POISN: poisson’s ratio

THERMAL: coefficient of linear thermal expansion

DEN: weight per unit volume

1. Orthoropic: for orthotropic material

Ex, Ey, Ez: modulii of elasticity in the corresponding directions

Tx, Ty, Tz: coefficients of linear thermal expansion in the

corresponding directions

Sxy, Sxz, Syz: shear modulii of elasticity in the corresponding

directions

Pxy, Pxz, Pyz: poisson’s ratios in the corresponding directions

*MATL-COLOR

Color data for materials

; iMAT, W_R, W_G, W_B, HF_R, HF_G, HF_B,

HE_R, HE_G, HE_B, bBLEND, FACT

iMAT: material number

W_R: red color number when displaying in Wire Frame

W_G: green color number when displaying in Wire Frame

W_B: blue color number when displaying in Wire Frame

HF_R: red color number of Hidden treated surface

HF_G: green color number of Hidden treated surface

HF_B: blue color number of Hidden treated surface

HE_R: red color number of the outline of Hidden treated surface

HE_G: green color number of the outline of Hidden treated surface

HE_B: blue color number of the outline of Hidden treated surface

bBLEND: assigns color transparency

(YES/NO) {NO}

FACT: factor (degree) of color transparency {0.5}

*TDM-FUNC (Time Dependent Material Function)

Creep/Shrinkage function of concrete

; FUNC=NAME, FTYPE, SCALE, CTYPE, ELAST

 DESC                                                 ; line 1

; DAY1, VALUE1, DAY2, VALUE2,?           ; from line 2

NAME: function name that defines Creep (Shrinkage)

FTYPE: function type

= CREEP: creep of concrete

= SHRINK: shrinkage of concrete

SCALE: scale factor

CTYPE: creep function data type

= SC: Specific Creep

= CF: Creep Compliance

= CC: Creep Coefficient

ELAST: modulus of elasticity of concrete

DESC: brief description

DAY1: time

VALUE1: creep /shrinkage data value

 

*TDM-TYPE (Time Dependent Material)

Time dependent material data (creep, shrink)

; NAME=NAME, CODE, STR, HU, VOL, AGE, TYPE, [ACI1],

[ACI2]                                          ; CODE=ACI

; NAME=NAME, CODE, STR, HU, MSIZE, CTYPE, AGE

; CODE=CEB, KS

; NAME=NAME, CODE, N1, PHI1, N2, PHI2

; CODE=MEM

; NAME=NAME, CODE, STR, HU, USS, UCS, VOL, RR

MOD                                            ; CODE=PCA

; NAME=NAME, CODE, STR, HU, VOL, UCS, VSR1, LAF

VSR, PST, bRCE, RR, MOD               ; CODE=COMBINED

; NAME=NAME, CODE, STR, HTYPE, HU, MSIZE

CTYPE, AGE                                  ; CODE=JAPAN

; NAME=NAME, CODE, STR, HTYPE, HU, MSIZE

AGE                                              ; CODE=CHINA

; NAME=NAME, CODE, bSSF, SSFNAME

; CODE=USER (line 1)

; CREEPFUNC1, AGE1, CREEPFUNC2, AGE2, ...

; USER (from line 2)

; [ACI1]: CURE, SLUMP, FAP, AIR, CC

; [ACI2]: UCC, USS

1. Common Items

NAME: Time dependent material name

CODE: DB of time dependent material

=ACI: American Concrete Institute

= KS: Korean Standard

= MEM: Modify Elasticity Modulus, consider creep by

modifying the elasticity of modulus.

= JAPAN: Japanese Standard

= CHINA: Chinese Standard

= USER: user directly specifies material data

 

2. In the case of  ACI

STR: 28 day compressive strength

HU: relative humidity

VOL: volume-surface area ratio

AGE: start time of shrinkage after casting concrete

TYPE: ultimate factor reflecting the properties of concrete

 

3. In the case of CEB, KS

MSIZE: notational size of structure

CTYPE: type of cement

= RS: Rapid hardening high strength cement

= NR: Normal or rapid hardening cement

= SL: Slowly hardening cement

 

4. In the case of MEM

N1: number of days between 0 (day) & N1 (day)

PHI1: reduction factor for modulus of elascity

 

5. In the case of PCA

STR: 28 day compressive strength

HU: relative humidity

USS: ultimate shrinkage strain

UCS: ultimate creep strain

VOL: volumn-surface area ratio

RR: reinforcement ratio of column

MOD: modulus of elasticity of reinforcement

 

6. In the case of COMBINED

STR: 28 days compressive strength

HU: relative humidity

VOL: volumn-surface area ratio

UCS: ultimate creep strain

VSR1: volumn-surface area ratio

LAF: age factor calculation

US: ultimate shrinkage strain

VSR: volumn-surface area ratio

PST: state of progress of shrinkage

bRCE: whether or not the reinforced concrete effect by PCA is

applied

RR: reinforcement ratio of column

MOD: modulus of elasticity of reinforcement

 

7. In the case of JAPAN

STR: 28 day compressive strength

HTYPE: type of curing

= CM: water-immerced curing

= RM: ambient curing

HU: relative humidity

MSIZE : notational size of structure

CTYPE: type of cement

= RN: rapid hardening Cement

= NC: normal Cement

AGE: start time of shrinkage after casting concrete

[ACI1] or [ACI2]

CURE: initial curing method

SLUMP: concrete slump value

FAP: fine aggregate ratio

AIR: air entraintment quantity

CC: cement quantity

UCC: ultimate creep coefficient

USS: ultimate shrinkage strain

 

8. In the case of CHINA

STR: 28 day compressive strength

HTYPE: type of curing

= CM: water-immerced curing

= RM: ambient curing

HU: relative humidity

MSIZE: notational size of structure

AGE: start time of shrinkage after casting

 

9. In the case of USER

bSSF: whether or not Shrinkage Strain Function is applied

SSFNAME: shinkage function to be applied

CREEPFUNC1: creep function to be applied

AGE1: age (elapsed time) at the time of load application

*TDM-ELAST

Time Dependent Material (Comp. Strength)

Change of Modulus of Elasticity (compressive

strength) relative to concrete maturity (age)

; NAME=NAME, TYPE, CODE, STRENGTH, A, B

; TYPE=CODE (Korean Standard, ACI)

; NAME=NAME, TYPE, CODE, STRENGTH, iCTYPE

; TYPE=CODE (CEB-FIP, Ohzagi)

; NAME=NAME, TYPE, CODE, STRENGTH

; TYPE=CODE (Chinese Standard)

; NAME=NAME, TYPE, SCALE

; TYPE=USER (line 1)

; DAY1, VALUE1, DAY2, VALUE2, ...

; USER (from line 2)

1. Common Items

NAME: function name that defines the change of Modulus of

Elasticity (compressive strength) relative to concrete maturity

TYPE: input method for the change of Modulus of Elasticity

(compressive strength)

=CODE: select concrete specs defined in the code

= USER: user directly specifies the change of Modulus

Elasticity

CODE: selected code name

=ACI

= CEB-FIP

= Ohzagi

= Chinese Standard

= Korean Standard

 

2.In the case of KS,

STRENGTH: concrete compressive strength relative to curing

time

=KS: concrete compressive strength at 91 days

=ACI: concrete compressive strength at 28 days

A,B: factors for compressive strength of concrete

 

3.In the case of CEB-FIP, Ohzagi

iCTYPE: different types of cement modulus

= 1: Rapid hardening high strength cement

= 2: Normal or rapid hardening cement

= 3: Slowly hardening cement

= 4: In cases of using flyash

 

4. In the case of USER

SCALE: scale factor

DAY1: time

VALUE1: data value of elastic modulus

*TDM-LINK (Time Dependent Material Link)

Assigns time dependent properties of materials to the

initially entered normal material data

; iMAT, TDM-TYPE1 (CREEP/SHRINKAGE),

TDM-TYPE2 (ELASTICITY)

iMAT: material number, which assigns time dependent properties

TDM-TYPE1 (CREEP/SHRINKAGE): selects a material

property, which has been defined in the Time Dependent Material

(Creep/Shrinkage)

TDM-TYPE2 (ELASTICITY) :

selects a material, which has been defined in the Time Dependent

Material (Elasticity)

*ELEM-DEPMATL (Change Element Dependent Material Property)

Modifies Notational size (h), which is applied in the

automatic calculation of time dependent property

; ELEM_LIST, H

ELEM_LIST: list of element numbers to be changed

H: geometric shape factor (h, Notational Size of Member

*SECTION (Section)

Section data of truss or beam elements

; iSEC, TYPE, SNAME, OFFSET, SHAPE, [DATA]

{, CCSHAPE}                           ; DB/USER

; iSEC, TYPE, SNAME, OFFSET, SHAPE, BLT, D1, D2, D3

D4, D5, D6                                ; 1st line - VALUE

; AREA, ASy, ASz, Ixx, Iyy, Izz      ; 2nd line

; CyP, CyM, CzP, CzM, QyB, QzB, PERI_OUT, PERI_IN,

Cy, Cz                                       ; 3rd line

; iSEC, TYPE, SNAME, OFFSET, SHAPE,

iREPLACE, ELAST, DEN, POIS, POIC   ; 1st line - SRC

; D1, D2, [DATA]                                ; 2nd line

; iSEC, TYPE, SNAME, OFFSET, SHAPE, 1, DB, NAME1

NAME2, D1, D2                                 ; COMBINED

; iSEC, TYPE, SNAME, OFFSET, SHAPE, 2, D11, D12,

D13, D14, D15, D21, D22, D23, D24]

; iSEC, TYPE, SNAME, OFFSET, SHAPE, iyVAR, izVAR

STYPE                          ; 1st line - TAPERED

;      DB,NAME1,NAME2        ; 2nd line(STYPE=DB)

;      [DIM1], [DIM2]               ; 2nd line (STYPE=USER)

;      D11, D12, D13, D14, D15, D16

; 2nd line (STYPE=VALUE)

;      AREA1, ASy1, ASz1, Ixx1, Iyy1, Izz1

; 3rd line (STYPE=VALUE)

;      CyP1, CyM1, CzP1, CzM1, QyB1, QzB1, PERI_OUT1,

PERI_IN1, Cy1, Cz1         ; 4th line (STYPE=VALUE)

;      D21, D22, D23, D24, D25, D26

; 5th line (STYPE=VALUE)

;      AREA2, ASy2, ASz2, Ixx2, Iyy2, Izz2

; 6th line (STYPE=VALUE)

;      CyP2, CyM2, CzP2, CzM2, QyB2, QzB2, PERI_OUT2

PERI_IN2, Cy2, Cz2                 ; 7th line (STYPE=VALUE)

[DATA]: 1, DB, NAME or 2, D1, D2, D3, D4, D5, D6

; [DIM1], [DIM2] : D1, D2, D3, D4, D5, D6

1. Common Items

iSEC: section number

TYPE: type of section property

= DBUSER: selected from DB or standard section

= VALUE: directly specified section property data

= SRC: section property of SRC member

=COMBINED: section property of combined sections

SNAME: section name

SHAPE: shape symbol of section (refer to Table 1 below)

 

2. DB/USER

CCSHAPE: cold formed section data

 

3. In the case of VALUE

   BLT: classifies builtup methods of members

   D1~D6: dimensions of section  

   AREA~Cz: section stiffness data

*refer to on-line manual

 

4. In the case of SRC

iREPLACE: reference material used for calculating the

stiffness of composite sections

=1: Steel        =2: Concrete

ELAST: ratio of modulus of elasticity of steel to concrete

DEN: ratio of steel density to concrete

POIS: poisson’s ratio for steel

POIC: poisson’s ratio for concrete

D1, D2: dimensions of a concrete section

 

7. COMBINED

 1: selecting a section from DB

   DB: DB of standard sections

NAME1, NAME2: names of two section types, which  make

up the combined section

D1: 1st dimension of a section

D2: 2nd dimension of a section

2: when ispecifying the main dimensions of standardized sections

(USER)

   D11: 1st dimension of a section

   D12: 2nd dimension of a section

   D13: 3rd dimension of a section

   D14: 4th dimension of a section

   D15: 5th dimension of a section

   D16: 6th dimension of a section

   D21: 7th dimension of a section

   D22: 8th dimension of a section

   D23: 9th dimension of a section

   D24: 10th dimension of a section

   D25: 11th dimension of a section

   D26: 12th dimension of a section

 

8. TAPERED

iyVAR: method of calculating moment of inertia about the y-axis

of the element local coordinate system {1}

= 1: 1st (Linear)

= 3: 3rd (Cubic)

izVAR: method of calculating moment of inertia about the z-axis

of the element local coordinate system {1}

= 1: 1st (Linear)

= 2: 2nd (Parabolic)

= 3: 3rd (Cubic)

STYPE: assigns the section type of a tapered section member to

be used

 

L

Angle

C

Channel

I

I-Section

T

T-Section

B

Box

P

Pipe

2L

Double Angle

2C

Double Channel

SB

Solid Rectangle

SR

Solid Round

CC

Cold Formed Channel

 

 

Table 1. Shape symbols of input sections (SNAME)

*SECT-COLOR

Color data of sections

; iSEC, W_R, W_G, W_B, HF_R, HF_G, HF_B, HE_R, HE_G,

HE_B, bBLEND, FACT

iSEC: section number

W_R: red color number when displaying in Wire Frame

W_G: green color number when displaying in Wire Frame

W_B: blue color number when displaying in Wire Frame

HF_R: red color number of Hidden treated surface

HF_G: green color number of Hidden treated surface

HF_B: blue color number of Hidden treated surface

HE_R: red color number of the outline of Hidden treated surface

HE_G: green color number of the outline of Hidden treated surface

HE_B: blue color number of the outline of Hidden treated surface

bBLEND: assigns color transparency

(YES/NO) {NO}

FACT: factor (degree) of color transparency {0.5}

*SECT-SCALE (Section Stiffness Scale Factors)

Stiffness scale factors applicable to the section

properties of line elements

; iSEC, AREA_SF, ASY_SF, ASZ_SF, IXX_SF, IYY_SF,

IZZ_SF, WGT_SF

iSEC: section subject to scale factors

AREA_SF: scale factor for section area

ASY_SF: scale factor for effective section area, which resists the y-

axis direction shear force in the element local coordinate system

ASZ_SF: scale factor for effective section area, which resists the z-

axis direction shear force in the element local coordinate system

IXX_SF: scale factor for torsional moment of inertiaa

IYY_SF: scale factor for moment of inertia about the y-axis in the  

element local coordinate system

IZZ_SF: scale factor for moment of inertia about the z-axis in the  

element local coordinate system

WGT_SF: scale factor for section weight

*TS-GROUP (Tapered Section Group)

Grouping Tapered Section members

; NAME, ELEM_LIST, ZVAR, ZEXP, ZFROM, ZDIST,

YVAR, YEXP, YFROM, YDIST

NAME: group name of tapered section

ELEM_LIST: element numbers included in the tapered section group

ZVAR: defines the change of section shape in the z-axis direction of the element local coordinate system

= Linear: linear change following a straight line

= Quadratic: Quadratic change following a 2 dimensional curve

ZEXP: assigns the exponent (1~2) of the function defining the  shape change of section

ZFROM: origin point for defining the mirror plane

ZDIST: distance from the origin point to the mirror plane in the x-

direction of the element local coordinate system

YVAR: defines the change of section shape in the y-direction of

 the element local coordinate system

*THICKNESS (Thickness)

Thickness data for planar elements

; iTHK, TYPE, bSAME, THIK-IN, THIK-OUT                     

; TYPE=VALUE

; iTHK, TYPE, SUBTYPE, RPOS, WEIGHT                   

 ; TYPE=STIFFENED, SUBTYPE=VALUE

;      SHAPE, THIK-IN, THIK-OUT, HU, HL                      

; for yz section

;      SHAPE, THIK-IN, THIK-OUT, HU, HL                    

 ; for xz section

; iTHK, TYPE, SUBTYPE, RPOS, PLATETHIK                    

 ; TYPE=STIFFENED, SUBTYPE=USER

;      bRIB {, SHAPE, DIST, SIZE1, SIZE2, ..., SIZE6}

                    ; for yz section

;      bRIB {, SHAPE, DIST, SIZE2, SIZE2, ..., SIZE6}                  

  ; for xz section

; iTHK, TYPE, SUBTYPE, RPOS, PLATETHIK, DBNAME                     

 ; TYPE=STIFFENED, SUBTYPE=DB

;      bRIB {, SHAPE, DIST, SNAME}                            

 ; for yz section

;      bRIB {, SHAPE, DIST, SNAME}                            

; for xz section

1. Common Items

iTHK: thickness ID number

TYPE: method of defining thickness data

=VALUE

2.

=STIFFENED

 

2. If Type is ‘Value’

bSAME: applies the same thickness to both in-plane and out-of-             

plane (bending) thicknesses (YES/NO) {YES}

THIK-IN: thickness applied to calculate the in-plane stiffness

THIK-OUT: thickness applied to calculate the out-of-plane stiffness

 

3. If Type is ‘Stiiffered’ and Subtype is‘Value’

SUBTYPE: method of defining the thickness data

  = VALUE  

 = USER   

= DB

RPOS: rib position

= LOWER  

= UPPER

WEIGHT: equivalent thickness data for weight calculation  

SHAPE: selects the rib section  

THIK-IN: thickness applied to calculate the in-plane stiffness  

THIK-OUT: thickness applied to calculate the out-of-plane stiffness

 

4. If Type is ‘Stiiffered’ and Subtype is ‘User’  

SUBTYPE, RPOS: refer to #3    

PLATETHIK: thickness data of plate element    

bRIB: selects whether or not ribs exist  

SHAPE: assigns the section shape of the rib  

DIST: distance (spacing) between the ribs   

SIZE1~ SIZE6: section size of the rib

5. If Type is ‘Stiiffered’ and Subtype is ‘DB’

SUBTYPE, RPOS: refer to #3

PLATETHIK: thickness data of plate element   

DBNAME: name of DB   

bRIB: selects whether or not ribs exist

SHAPE: assigns the section shape of the rib

DIST: distance (spacing) between the ribs

SNAME: section name

*THIK-COLOR

Color data for individual thickness numbers

; iTHK, W_R, W_G, W_B, HF_R, HF_G, HF_B, HE_R, HE_G

HE_B, bBLEND, FACT

iTHK: thickness ID number

W_R: red color number when displaying in Wire Frame

W_G: green color number when displaying in Wire Frame

W_B: blue color number when displaying in Wire Frame

HF_R: red color number of Hidden treated surface

HF_G: green color number of Hidden treated surface

HF_B: blue color number of Hidden treated surface

HE_R: red color number of the outline of Hidden treated surface

HE_G: green color number of the outline of Hidden treated surface

bBLEND: assigns color transparency

(YES/NO) {NO}

FACT: factor (degree) of color transparency {0.5}

*THIK-COLOR

Color data for individual thickness numbers

; iTHK, W_R, W_G, W_B, HF_R, HF_G, HF_B, HE_R, HE_G,

 HE_B, bBLEND, FACT

iTHK: thickness ID number

W_R: red color number when displaying in Wire Frame

W_G: green color number when displaying in Wire Frame

W_B: blue color number when displaying in Wire Frame

HF_R: red color number of Hidden treated surface

HF_G:green color number of Hidden treated surface

HF_B: blue color number of Hidden treated surface

HE_R: red color number of the outline of Hidden treated surface

HE_G: green color number of the outline of Hidden treated surface

HE_B: blue color number of the outline of Hidden treated surface

bBLEND: assigns color transparency

(YES/NO) {NO}

FACT: factor (degree) of color transparency {0.5}

*TDN-PROPERTY (Tendon Property)

Tendon property and assigning the methods of

prestress application

; NAME, TYPE, MATL, AREA, DIA, RC, FF, WF, US, YS,

 LT, ASB, ASE,

NAME: name of tendon to be defined

TYPE: type of tendon classified by the location of the tendon

relative to the element section

= Internal: located within the section

= External: located outside of the section

AREA: total area of the tendon

DIA: diameter of the duct

RC: C, Relaxation Coefficient

FF: Friction Factor

WF: Wobble Factor

US: Ultimate Strength

YS: Yield Strength

LT: method of tensioning

= Pretension

 = Post-tension

ASB: magnitude of slip at the tensioning anchorage

ASE: magnitude of slip at the end anchorage

*TDN-PROFILE (Tendon Profile)

Placing arrangement and defining the shape of

 tendon relative to the element section

; NAME=NAME, TDN-PROPERTY, ELEM_LIST, BEGIN

END, CURVE                 ; line 1;

;      SHAPE, IP_X, IP_Y, IP_Z, AXIS, VX, VY

                                    ; line 2 (SHAPE=STRAIGHT)

; SHAPE, IP_X, IP_Y, IP_Z, RC_X, RC_Y, OFFSET

                                    ; line 2 (SHAPE=CURVE)

;      XAR_ANGLE, bPROJECTION, GR_AXIS,

       GR_ANGLE            ; line 3

;       X1, Y1, Z1, bFIX1, RY1, RZ1, RADIUSI                                   

 ; from line 4

;       ...

;       Xn, Yn, Zn, bFIXn, RYn, RZn, RADIUSn

NAME: tendon name

TDN-PROPERTY: assigns tendon properties

ELEM_LIST: element numbers for tendon assignment

BEGIN: straight distance of the tendon at the beginning

END: straight distance of the tendon at the end

CURVE: curved shape of tendon

= SPLINE  

= ROUND

 

1. In the case of STRAIGHT

SHAPE: shape of the imaginary axis, which is referenced for  

placing the straight tendon

IP_X: X-coordinate of Profile Insertion Point

IP_Y: Y-coordinate of Profile Insertion Point

IP_Z: Z-coordinate of Profile Insertion Point

AXIS: defines the x-axis direction in the tendon coordinate

system if the tendon is placed straight

VX: x-axis is parallel with the X-axis of the global coordinate system

VY: x-axis is parallel with the Y-axis of the global coordinate system

 

2. In the case of CURVE

SHAPE: shape of the imaginary axis, which is referenced for  placing the curved tendon

IP_X: X-coordinate of Profile Insertion Point

IP_Y: Y-coordinate of Profile Insertion Point

IP_Z: Z-coordinate of Profile Insertion Point

RC_X: center x-coordinate of the reference circle in the global

coordinate system if tendon is placed curvilinearly

RC_Y: center y-coordinate of the reference circle in the

coordinate system if tendon is placed curvilinearly

OFFSET: places the tendon in the location projected in the

direction of the radius of the circle

XAR_ANGLE: rotation angle about the x-axis in the tendon

coordinate system (convenient when placing sloped web tendons)

bPROJECTION: defines whether or not to place the tendon at

the location projected onto the plane after rotation (YES/NO)

GR_AXIS: reference axis about which is rotated

GR_ANGLE: rotation angle about the Y or Z axis in the global coordinate system

X1: X-coordinate of the point through which the tendon passes

 based on the tendon coordinate system

Y1: Y-coordinate of the point through which the tendon passes  

based on the tendon coordinate system

Z1: Z-coordinate of the point through which the tendon passes  

based on the tendon coordinate system

bFIX1: whether or not to fix the tangent angle of the tendon

(YES/NO)

RY1: tangent angle relative to the x-axis in the

 x-z plane in the tendon coordinate system when the tangent angle is fixed

RZ1: tangent angle relative to the x-axis in the

x-y plane in the tendon coordinate system when the tangent angle is fixed

RADIUS: radius of the circle in tangent with the straight line oftendon

*CONSTRAINT(Supports)

Conditions restraining the nodal degrees of freedom

; NODE_LIST, CONST (Dx, Dy, Dz, Rx, Ry, Rz), GROUP

NODE_LIST: node number

CONST (Dx, Dy, Dz, Rx, Ry, Rz): components of degrees of

freedom identified in 6 Digit

CodeGROUP: Boundary Group Name

 

*SPRING (Point Spring Supports)

Elastic support conditions assigned to nodes

; NODE_LIST, SDx, SDy, SDz, SRx, SRy, SRz, GROUP

NODE_LIST: node number

SDx: spring constant in the x-axis direction [force/length]

SDy: spring constant in the y-axis direction [force/length]

SDz: spring constant in the z-axis direction [force/length]

SRx: rotational spring constant about the x-axis direction

[moment/angle]

SRy: rotational spring constant about the y-axis direction

 [moment/angle]

SRz: rotational spring constant about the z-axis direction

[moment/angle]

GROUP: Boundary Group Name

*GSPRTYPE (Define General Spring Supports)

Stiffness of a general support spring

; NAME, SDx1, SDy1, SDy2, SDz1, SDz2, SDz3, ...,

 SRz1, ..., SRz6

NAME: name of spring stiffness

SDx1: spring stiffness in the global or local x-axis direction

SDy1, SDy2: spring stiffness interrelated in the global or local x-

and y-axis directions

SDz1, SDz2, SDz3: spring stiffness interrelated in the global or

local x-, y- and z-axis directions

SRz1, ? SRz6: rotational spring stiffness interrelated in

the global or local x-, y- and z-axis directions

*GSPRING (General Spring Supports)

Conditions of a general spring support assigned to nodes

; NODE_LIST, TYPE-NAME, GROUP

NODE_LIST: node number

TYPE-NAME: name of General Spring Type

GROUP: Boundary Group Name

*ELASTICLINK

Elastic link elements connecting two nodes

; iNODE1, iNODE2, Link, ANGLE, SDx, SDy, SDz, SRx, SRy,

SRz, DRy, DRz, GROUP              ; GEN

; iNODE1, iNODE2, Link, ANGLE, bSHEAR, DRy, DRz,

GROUP                                   ; RIGID

; iNODE1, iNODE2, Link, ANGLE, SDx, bSHEAR, DRy, DRz

GROUP                                   ; TENS, COMP

iNODE1: 1st node number of an elastic link

iNODE2: 2nd node number of an elastic link

Link: assigns the type of the elastic link element {GEN}

= GEN: directy uses the stiffness values that the user specifies

= RIGID: ridgid link stiffness automatically assigned by the  program

= TENS: uses as a tension-only element

= COMP: uses as a compression-only element

ANGLE: Beta Angle of the elastic link element

SDx: spring constant in the x-axis direction [force/length]

SDy: spring constant in the y-axis direction [force/length]

SDz: spring constant in the z-axis direction [force/length]

SRx: rotational spring constant about the x-axis direction

[moment/angle]

SRy: rotational spring constant about the y-axis direction

[moment/angle]

SRz: rotational spring constant about the z-axis direction

[moment/angle]

bSHEAR: whether or not to assign the location of shear spring

DRy, DRz: location of shear spring in the ratio of element length

GROUP: Boundary Group Name

*NL-PROP (Nonlinear Link Property)

Joint conditions of beam ends

; NAME, TYPE, TW, bSSL, DY, DZ, DESC

; bLDX, DX, bNDX, [NL_PROP]

; bLDY, DY, bNDY, [NL_PROP]

; bLDZ, DZ, bNDZ, [NL_PROP]

; bLRX, RX, bNRX, [NL_PROP]

; bLRY, RY, bNRY, [NL_PROP]

; bLRZ, RZ, bNRZ, [NL_PROP]

; [NL_PROP]: DSTIFF, DAMP, DEXP, bRIGDBR, BSTIFF,

EFFDAMP              ; Visco-elastic Damper Type

; [NL_PROP]: STIFF, OPEN, EFFDAMP                    

           ; Gap Type or Hook Type

; [NL_PROP]: STIFF, YSTR, PYS_RATIO, YEXP, PA

EFFDAMP              ; Hysteretic System Type

; [NL_PROP]: STIFF, YSTR, PYS_RATIO, PA, PB,

EFFDAMP              ; Lead Rubber Bearing Type

; [NL_PROP]: STIFF, FCS, FCF, RP, RADIUS, PA, PB,

EFFDAMP              ; Friction Pendulum System Type

1. Common Items

NAME: Property name of nonlinear link

TYPE: Type of nonlinear link

 = VD: Viscoelastic Damper

 = GAP: Gap

 = HOOK: Hook

 = HS: Hysteretic System

 = LRBI: Lead Rubber Bearing Isolator

 = FPSI: Friction Pendulum System Isolator

TW

bSSL

DY

DZ

DESC

*NL-LINK (Nonlinear Link)

Joint conditions of beam ends

; iNODE1, iNODE2, PROP, ANGLE, GROUP

iNODE1

iNODE2

PROP

ANGLE

GROUP

*FRAME-RLS (Beam End Release)

Joining conditions of bean ends

; ELEM_LIST, FLAG-i, Fxi, Fyi, Fzi, Mxi, Myi, Mzi

                                                ; 1st Line

;       FLAG-j, Fxj, Fyj, Fzj, Mxj, Myj, Mzj, GROUP

                                                ; 2nd Line

1st Line

ELEM_LIST: element number

FLAG-i: i-node of a beam element

Fxi: release axial force of the i-node

Fyi: release y-direction shear force at the i-node in the element local

 coordinate system

Fzi: release z-direction shear force at the i-node in the element local

coordinate system

Mxi: release torsional moment at the i-node

Myi: release moment about y-direction at the i-end in the element local

coordinate system

Mzi: release moment about z-direction at the i-end in the element local

coordinate system

2nd Line

FLAG-j: j-node of a beam element

Fxj: release axial force of the j-node

Fyj: release y-direction shear force at the j-node in the element local

coordinate system

Fzj: release z-direction shear force at the j-node in the element local

coordinate system

Mxj: release torsional moment at the j-node

Myj: release moment about y-direction at the j-end in the element local

coordinate system

Mzj: release moment about z-direction at the j-end in the element local

coordinate system

Note: Partial Fixity may be entered as required

*OFFSET (Beam End Offsets)

Rigid end offset or eccentricity at the beam ends

; ELEM_LIST, TYPE, RGDXi, RGDYi, RGDZi, RGDXj

RGDYj, RGDZj, GROUP             ; TYPE=GLOBAL

; ELEM_LIST, TYPE, RGDi, RGDj, GROUP

                                                ; TYPE=ELEMENT

ELEM_LIST: element number

TYPE: type of coordinate system

= GLOBAL: offset distances in vectors in the global coordinate

system with respect to the distances and directions from the node to the Offset

 = ELEMENT: offset distance relative to the x-direction of the

element local coordinate system

In the case of GLOBAL

RGDXi: offset distance in vector in the global X-direction at the node

RGDYi: offset distance in vector in the global Y-direction at the i-node

RGDZi: offset distance in vector in the global Z-direction at the i-node

RGDXj: offset distance in vector in the global X-direction at the j-node

RGDYj: offset distance in vector in the global Y-direction at the j-node

RGDZj: offset distance in vector in the global Z-direction at the j-node

GROUP: Boundary Group Name

In the case of ELEMENT

RGDi: offset distance from the i-node in the (+) x-direction of the

element local coordinate system

RGDj: offset distance from the j-node in the

(-) x-direction of the element local coordinate system

GROUP: Boundary Group Name

*PLATE-RLS (Plate End Release)

Node connecting condition (Hinge, Fixed Joint) and

Partial Fixity in a plate element

; ELEM_LIST, N1, N2, N3, N4, GROUP

ELEM_LIST: element number

N1:

 Fx (Fy): releases axial stiffness in the x (y) axis direction in the

element local coordinate system

Fz: releases shear stiffness in the z-direction in the element local

coordinate system

Mx: releases bending stiffness about the x-axis in the

element  local coordinate system

 My: releases bendding stiffness about the y-axis in the

element local coordinate system

N2, N3, N4: same as N1

GROUP: Boundary Group Name

* Can assign Partial Fixity if required

 

*RIGIDLINK (Rigid Link)

Link conditions of master and slave nodes

; M-NODE, DOF, S-NODE LIST, GROUP

M-NODE: Master Node number

DOF: signal for specifying components of constrained degrees of freedom    

(composed of a 6 Digit Code using "1" or "0")

S-NODE LIST: list of Slave Node numbers

GROUP: Boundary Group Name

*PANEL-ZONE

Offset distance due to Panel Zone

; bCALC, FACTOR, iPOSITION

bCALC: whether to automatically consider rigid end offset

(YES/NO) {YES}

FACTOR: correction factor for rigid end offst

iPOSITION: output location of member forces

*LOCALAXIS (Node Local Axis)

Used to input boundary conditions by defining a

nodal coordinate system at a specific node or produce

reaction output in the nodal corrdinate system

; NODE_LIST, iMETHOD, ANGLE-x, ANGLE-y, ANGLE-z

                                                 ; iMETHOD=1

; NODE_LIST, iMETHOD, P0X, P0Y, P0Z, P1X, P1Y, P1Z

P2X, P2Y, P2Z                             ; iMETHOD=2

; NODE_LIST, iMETHOD, V1X, V1Y, V1Z, V2X, V2Y, V2Z

                                                ; iMETHOD=3

NODE_LIST: node number

iMETHOD: input method of nodal coordinate system {1}  

1 = Angle: defines the nodal coordinate system by specifying 3rotation angles  

2 = 3 Points: defines the nodal coordinate system by specifying 3node coordinates

3 = Vector: defines the nodal coordinate system by specifying 2vectors

1. In the case of Angle

ANGLE-X: rotational angle about the X-axis of the GCS

ANGLE-y: rotational angle about y’-axis rotated about the X-axis

ANGLE-z: rotational angle about z’’-axis rotated about X and y’ axes

 

2. IN the case of 3 Point

P0X, P0Y, P0Z: coordinates of origin in a nodal coordinate system

P1X, P1Y, P1Z: coordinates of a specific point on the x-axis in NCS

P2X, P2Y, P2Z: coordinates of a specific point moved

parrallel with the y-axis from P1 in NCS

3. In the case of Vector

V1X, V1Y, V1Z: x-axis direction vector from the origin of NCS

V2X, V2Y, V2Z: vector from the origin of NCS of a point moved

by a specific distance parrallel with the y-axis of NCS from the end point of V1

*STORY-DGROUP (Story Diaphgram Group for Construction Stage)

Assign the Strory Diaphragm information defined automatically

by the Story function to boundary condition group

; STORY, GROUP

STORY: story name

GROUP: Boundary Group Name

 

*STLDCASE (Static Load Cases)

; LCNAME, LCTYPE, DESC

LCNAME: name of unit load case

LCTYPE: type of unit load case

USER = User Defined Load  

D = Dead Load

L = Live Load

LR=Roof Live Load  

W = Wind Load on Structure

E = Earthquake

S = Snow Load  

R = Rain Load

IP = Ice Pressure  

EP = Earth Pressure

WP = Ground Water Pressure

FP = Fluid Pressure

SF = Stream Flow Pressure

B = Buoyancy

CR = Creep

SH = Shrinkage

T = Temperature

PS = Prestress

CS = Construction Stage Load

ER = Erection Load

IL = Live Load Impact

BK = Longitudinal Force from Live Load

WL = Wind Load on Live Load

CF = Centrifugal Force

CO = Collision Load  

TPG = Rib Shortening

DESC: description of load case

*BLDG-CTRL (Building Control Data)

Nodal mass data assigned to nodes

; bBASE, bMASS, bCENTER, USE

                                          ; Line 1

; LCNAME1, FACT1, LCNAME2, FACT2,?/p>

 YES, 20, YES, YES, LOAD

 1, 1

bBASE: whether or not to apply the height of ground surface base

LEVEL: height of ground surface base

bMASS: whether or not to include the mass below the base for

eigenvalue analysis

bCENTER: whether or not to calculate the center of floor

USE: selects the method of calculating the floor center  

= MASS: calculates the floor center using the distribution of mass  

= LAOD: calculates the floor center using static (long term) loads

If ?span style="font-weight: bold;">LOAD?/span> is selected for USE

LCNAME1: load case

FACT1: scale factor

*STORY (Story)

Story data (Defined by Z-coordinate)

; NAME, LEVEL, bFLDIAP, WINDWX, WINDWY,

WINDCX, WINDCY, ECCX, ECCY

NAME: story name

LEVEL: global Z-direction coordinate

bFLDIAP: whether or not to apply the Diaphragm function to the

corresponding story (YES/NO)

WINDWX: effective width in the X-direction subjected to Y-direction wind load

WINDWY: effective width in the Y-direction subjected to Y-direction wind load

WINDCX: X-direction coordinate of the point of wind load application

WINDCY: Y-direction coordinate of the point of wind load application

ECCX: X-directional eccentricity to calculate torsional moment due to the

story seismic load in the Y-direction

ECCY: Y -directional eccentricity to calculate torsional moment due to the

story seismic load in the X-direction

 

*NODALMASS (Nodal Masses)

Nodal mass data assigned to nodes

; NODE_LIST, mX, mY, mZ, rmX, rmY, rmZ

NODE_LIST: node numbers

mX: concentrated mass in the X-direction in the GCS

mY: concentrated mass in the Y-direction in the GCS

mZ: concentrated mass in the Z-direction in the GCS r

mX: rotaional concentrated mass about the X-direction in GCS

rmY: rotaional concentrated mass about the Y-direction in GCS

rmZ: rotaional concentrated mass about the Z-direction in GCS

*DIAP-MASS (Floor Diaphragm Masses)

Floor mass data assigned to a specific story in a building structure

; 1, SSTORY, ESTORY, MP, MA, XC, YC

                                            ; point

; 2, SSTORY, ESTORY, ML, D1, XC, YC

                                            ; line

; 3, SSTORY, ESTORY, MA, X1, Y1, X2, Y2, X3, Y3

                                            ; triangle

; 4, SSTORY, ESTORY, MA, XC, YC, D1, D2

                                            ; rectangle

; 5, SSTORY, ESTORY, ML, XC, YC, D1, D2, D3

                                            ; circular arc;

6, SSTORY, ESTORY, MA, XC, YC, D1, D2, D3, D4

                                           ; circular area

SSTORY: story number for the starting story

ESTORY: story number for the ending story

 

A. In the case of entering data as Point Mass

MP: point mass component in the lateral directions [Mass]

MA: rotational mass moment of inertia about the Z-direction in GCS at the point mass

XC, YC: coordinates of the center of the point mass in GCS

 

B. In the case of entering data as Line Mass

ML: Mass per unit length (Mass/Length)

D1: length of the line mass

XC, YC: coordinates of the center of the line mass in GCS

 

C. In the case of entering data as Triangular Area Mass

MA: Mass per unit area (Mass/Area)

X1, Y1: coordinates of a corner of the triangular area

X2, Y2: coordinates of the second corner of the triangular area

X3, Y3: coordinates of the third corner of the triangular area

 

D. In the case of entering data as Rectangular Area Mass

MA: Mass per unit area (Mass/Area)

XC, YC: coordinates of the center of the rectangular area in GCS

D1: length of a side of the rectangle

D2: length of the side of the rectangle perpendicular to D1

 

E. In the case of entering data as Circular Arc Mass

ML: Mass per unit length (Mass/Length)

XC, YC: coordinates of the center of the circular arc in GCS

D1: angle of the circular arc (Degree)

D2: radius of the circular arc

D3: angle of inclination formed by the center of the mass of the circular

arc relative to GCS X-axis (Degree)

 

F. In the case of entering data as Circular Area (fan-shaped) Mass

MA: Mass per unit area (Mass/Area)

XC, YC: coordinates of the center of the circle encompassing the fan-

shaped circular area in GCS

D1: the inner angle of the circular fan-shaped area (Degree)

D2: radius of the fan-shaped area

D3: width of the fan-shaped area in the radial direction  

(D2=D3 if it is a full fan)

D4: angle of inclination formed by the center of the mass of the fan-

shaped circular area relative to GCS X-axis (Degree)

*LOADTOMASS (Loads to Masses)

Conversion of vertical loads into concentrated mass data

; *LOADTOMASS, DIR, bNODAL, bBEAM, bFLOOR,

bPRES, GRAV

; LCNAME1, FACTOR1, LCNAME2, FACTOR2, ...

                                              ; from line 1

DIR: assigns the directions in which the converted mass will be considered {XY}

bNODAL: option to convert nodal loads (YES/NO) {YES}

bBEAM: option to convert beam loads (YES/NO) {YES}

bFLOOR: option to convert floor loads (YES/NO) {YES}

bPRES: option to convert pressure loads (YES/NO) {YES}

GRAV: gravitational acceleration {9.806 m/sec2}

LCNAME1: selects the Load Case, which will be converted

FACTOR1: scale factor to be applied when loads are converted into mass {1}

*NAMEDPLANE (Named Plane)

Assignment of a name to a plane

; NAME, TYPE, TOL, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3

;NAME, TYPE, TOL, COORD

NAME: plane name

TYPE: selects the method of assigning the plane {1}

= 1 : 3-Point

= 2 : X-Y plane

= 3 : X-Z plane

= 4 : Y-Z plane

TOL: tolerance within which a plane is selected as the assigned plane {0.001 m}

X1, Y1, Z1: coordinates of the 1st point on the plane in GCS

X2, Y2, Z2: coordinates of the 2 nd point on the plane in GCS

X3, Y3, Z3: coordinates of the 3rd point on the plane in GCS

COORD: X, Y or Z coordinate in GCS for TYPE 2, 3 & 4

*NAMEDUCS (Named UCS)

Appllication of saved User Coordinate System previously assigned

; NAME, OX, OY, OZ, VXX, VXY, VXZ, VYX, VYY, VYZ

NAME: name of the saved UCS

OX: X-coordinate in GCS defining the origin of the selected UCS

OY: Y-coordinate in GCS defining the origin of the selected UCS

OZ: Z-coordinate in GCS defining the origin of the selected UCS

VXX: X-coordinate in GCS for the vector defining the x-axis

direction of the selected UCS

VXY: Y-coordinate in GCS for the vector defining the x-axis

direction of the selected UCS

VXZ: Z-coordinate in GCS for the vector defining the x-axis

direction of the selected UCS

VYX: X-coordinate in GCS for the vector defining the y-axis

 direction of the selected UCS

VYY: Y-coordinate in GCS for the vector defining the y-axis

direction of the selected UCS

VYZ: Z-coordinate in GCS for the vector defining the y-axis

direction of the selected UCS

*GROUP (Group)

Grouping desired entities by assigning a specific group name

; NAME, NODE_LIST, ELEM_LIST

NAME: Group name

NODE_LIST: selected node numbers

ELEM_LIST: selected element numbers

*BNDR-GROUP (Boundary Group)

Grouping nodes or elements constrained with

boundary conditions by assigning a specific boundary

group name

; NAME

NAME: Boundary Group name to be created, modified or deleted

*LOAD-GROUP (Load Group)

Grouping nodes or elements assigned with loads by

assigning a specific load group name

; NAME

NAME: Load Group name to be created, modified or deleted

*USE-STLD

Corresponding unit load case

USE-STLD: shows entered unit load cases and the coresponding loads

*SELFWEIGHT (Self Weight)

Applying the selfweight of the analysis model as loads

; *SELFWEIGHT, X, Y, Z, GROUP

X: weight scale factor for the X-direction component in GCS

Y: weight scale factor for the Y-direction component in GCS

Z: weight scale factor for the Z-direction component in

GCSGROUP: Group Name

*CONLOAD (Nodal Loads)

loads assigned to nodes

; NODE_LIST, FX, FY, FZ, MX, MY, MZ, GROUP

NODE_LIST: node numbers

FX: concentrated load component in the GCS X-direction

FY: concentrated load component in the GCS Y-direction

FZ: concentrated load component in the GCS Z-direction

MX: concentrated moment component about the GCS X-direction

MY: concentrated moment component about the GCS Y-direction

MZ: concentrated moment component about the GCS X-direction

GROUP: Group Name

*SPOISP (Specified Displacement of Supports)

Forced displacements of supports

; NODE_LIST, FLAG, Dx, Dy, Dz, Rx, Ry, Rz, GROUP

NODE_LIST: node numbers

FLAG: symbol of degree of freedom to which a specified

displacement will be specified      

(6 Digit Code using "1" or "0")

Dx: specified displacement component in the X-direction

Dy: specified displacement component in the Y-direction

Dz: specified displacement component in the Z-direction

Rx: specified rotational displacement component about the X-direction

Ry: specified rotational displacement component about the Y-direction

Rz: specified rotational displacement component about the Z-direction

GROUP: Group Name

*BEAMLOAD ( Element Beam Loads )

Beam loads applied to beam elements

; ELEM_LIST, CMD, TYPE, DIR, bPROJ, D1, P1, D2, P2, D3

P3, D4, P4, GROUP

ELEM_LIST: element numbers

CMD: load classification {BEAM}

= BEAM: Element Beam Load

= FLOOR: Floor Load

= LINE: Line Beam Load

= TYPICAL: Typical Loads

TYPE: load type {UNILOAD}

= CONLOAD: Concentrated Forces

= CONMOMENT: Concentrated Moments

= UNILOAD: Uniform Loads

= UNIMOMENT: Uniform Moments/Torsions

DIR: direction of load {GZ}

LX: X-direction in the element local coordinate system      

LY: Y-direction in the element local coordinate system

LZ: Z-direction in the element local coordinate system      

GX: about X-direction in GCS

GY: about Y-direction in GCS     

GZ: about Z-direction in GCS

bPROJ: option to specify projection of beam loads {NO}     

(not relevant to concentrated loads or concentrated moments)

D1: location of beam load on the beam element

P1: magnitude of the beam load

GROUP:Group Name

*FLOADTYPE(Define Floor Load Type )

Definition of floor load

; NAME, DESC                         ; 1st line

; LCNAME1, FLOAD1, bSBU1, ..., LCNAME4, FLOAD4,

                                   ; 2nd line

NAME: name of floor load

DESC: brief description

LCNAME1: name of unit load case

FLOAD1: magnitude of unit load

 option to to include the weight of dummy beam elements (

YES/NO)

 

*FLOAD-COLOR

Color data of floor loads

; NAME, W_R, W_G, W_B, HF_R, HF_G, HF_B, HE_R, HE_G

HE_B, bBLEND, FACT

NAME: name of floor load

W_R: red color number when displaying in Wire Frame

W_G: green color number when displaying in Wire Frame

W_B: blue color number when displaying in Wire Frame

HF_R: red color number of Hidden treated surface

HF_G: green color number of Hidden treated surface

HF_B: blue color number of Hidden treated surface

HE_R: red color number of the outline of Hidden treated surface

HE_G: green color number of the outline of Hidden treated surface

HE_B: blue color number of the outline of Hidden treated surface

bBLEND: assigns color transparency

(YES/NO) {NO}

FACT: factor (degree) of color transparency {0.5}

*FLOORLOAD (Floor Loads)

load (floor load) onto beam or

wall elements within an enclosed range

; LTNAME, iDIST, ANGLE, iSBEAM, SBANG, SBUW, DIR,

bPROJ, DESC, GROUP, NODE1, ..., NODEn

LTNAME: name of floor load

iDIST: method of distributing floor load {2}

= 1 : distributed in 1 direction

= 2 : distributed in 2 directions

= 3 : Polygon-Centroid

= 4 : Polygon-Length

ANGLE: angle of the direction of the load distribution {0}

iSBEAM: number of imaginary sub-beams placed in a sub-area {0}

SBANG: placement angle of the imaginary sub-beams {90}

SBUW: self-weight per unit length of a sub-beam [load/length] {0}

DIR: acting direction of floor load {GZ}

LX: X-direction in the local floor coordinate system      

LY: Y- direction in the local floor coordinate system     

LZ: Z-direction in the local floor coordinate system      

GX: X-direction in GCS      

GY: Y-direction in GCS      

GZ: Z-direction in GCS

bPROJ: option to specify projection of floor loads (YES/NO) {NO}

DESC: brief description

GROUP: Group Name

NODE1, ..., NODEn: node numbers identifying the floor load

*PRESTRESS (Prestress Beam Loads )

Prestress loads

; ELEM_LIST, LTYPE, TENS, DI, DM, DJ, GROUP

ELEM_LIST: element numbers

LTYPE: type of beam element prestress load {1}    

(not relevant to truss/tension-only/compression-only elements)

= PRE: process of prestress effect is considered

(Prestress condition)

= POST: condition after the prestress is considered

(Post-stress condition)

TENS: Prestress Tension Force

DI: Cable Drape in the ECS z-direction at the i-node of the beam element

DM: Cable Drape in the ECS z-direction at the center point of the beam element

DJ: Cable Drape in the ECS z-direction at the j-node of the beam element

GROUP: Load Group Name

*PRETENSION (Pretension Loads)

Pretension Loads

; ELEM_LIST, TENS, GROUP

ELEM_LIST : element numbers

TENS: Pretension Load

GROUP: Load Group Name

*FINISHINGLOADS (Finhing Material Loads)

Finishing Loads

; ELEM_LIST, COVERING-TYPE, FACE1, FACE2, FACE3,

FACE4, D, DENSITY, DIR, SCALE, GROUP

; *SYSTEMP*PRESSURE   ; Pressure Loads

; ELEM_LIST, CMD, ETYP, LTYP, DIR, VX, VY, VZ, bPROJ

PU, P1, P2, P3, P4, GROUP   ; ETYP=PLATE, LTYP=FACE

; ELEM_LIST, CMD, ETYP, LTYP, iEDGE, DIR, VX, VY, V

PU, P1, P2, GROUP            ; ETYP=PLATE, LTYP=EDGE

; ELEM_LIST, CMD, ETYP, iEDGE, DIR, VX, VY, VZ, PU, P1

P2, GROUP                      ; ETYP=PLANE

; ELEM_LIST, CMD, ETYP, iFACE, DIR, VX, VY, VZ, bPROJ,

PU, P1, P2, P3, P4, GROUP   ; ETYP=SOLID

; [PLATE] : plate, plane stress, wall, [PLANE]

: axisymmetric, plane strain

ER, SYSTEMP, GROUP

ELEM_LIST: element numbers

COVERING-TYPE: assigns the method of applying finishing loads

= ENVELOP

 = FILL

 = SURROOND

FACE 1~4: assigns the range of finishing material

 = FULL

 = HALF

D: thickness of finishing

DENSITY: unit weight of the finishing material

DIR: direction of the finishing material load

= Gx: X-direction in GCS

= Gy: Y-direction in GCS

= Gz: Z-direction in GCS

SCALE: scale factor for applying the finishing load

*PRESSURE (Pressure Loads)

Pressure loads

; ELEM_LIST, CMD, ETYP, LTYP, DIR, VX, VY, VZ, bPROJ

PU, P1, P2, P3, P4, GROUP   ; ETYP=PLATE, LTYP=FACE

; ELEM_LIST, CMD, ETYP, LTYP, iEDGE, DIR, VX, VY, VZ

PU, P1, P2, GROUP            ; ETYP=PLATE, LTYP=EDGE

; ELEM_LIST, CMD, ETYP, iEDGE, DIR, VX, VY, VZ, PU, P1

P2, GROUP                      ; ETYP=PLANE

; ELEM_LIST, CMD, ETYP, iFACE, DIR, VX, VY, VZ, bPROJ

PU, P1, P2, P3, P4, GROUP  ; ETYP=SOLID

; [PLATE] : plate, plane stress, wall, [PLANE]

: axisymmetric, plane strain

ER, SYSTEMP, GROUP

1. Common items

ELEM_LIST: element numbers

CMD: type of load

= PRES: Pressure Loads

= HYDRO: Hydrostatic Pressure Loads

ETYP: selects the type of element {PLATE}

= PLATE: Plate

= PLANE: Plane Stress, Plane Strain, Axisymmetric

 = SOLID: 8 Node-Solid, 6 Node-Solid, 4 Node-Solid

 

2. If  ETYPE is ‘PLATE’ and LTYPE is ‘FACE’

LTYPE: location of loading application {FACE}

DIR: direction of load application

= Lx, Ly, Lz: loading applied in x, y, z ditrections in ECS

= Gx, Gy, Gz: loading applied in X, Y, Z ditrections in GCS

= VECTOR: loading applied in the direction of the vector defined   

by User

Vx, Vy, Vz: X, Y, Z-direction distances defining the vector from the

reference point in GCS

bPROJ: option to specify projection of loads {NO}

PU: Uniformly distributed load value

P1~4: Linearly distributed load value

GROUP: Load Group name

 

3. If  ETYPE is ‘PLATE’ and LTYPE is ‘EDGE’

LTYPE: location of loading application {FACE}{EDGE}

iEDGE: element edge subjected to load application   

= 1 : EDGE #1

= 2 : EDGE #2

 = 3 : EDGE #3

= 4 : EDGE #4

: direction of load application

= NORMAL: loads applied in the direction paralleled with the

element face

*for others: refer to #2 above

 

4. If  ETYPE is ‘PLATE’

DIR: direction of load application

= NORMAL, Lx, Ly, Vector: refer to #2 & #3

 

5. If  ETYPE is ‘SOLID

iFACE: element face onto which the load is applied  

= 1 : Face #1  

= 2 : Face #2

= 3 : Face #3

 = 4 : Face #4

= 5 : Face #5

= 6 : Face #6

**for others: refer to #2, #3 & #4 above

*SYSTEMPER (System Temperature)

Final temperature in thermal stress analysis

; *SYSTEMPER, SYSTEMP, GROUP

SYSTEMP: final temperature of structure

GROUP: Load Group Name

*NDTEMPER (Nodal Temperatures )

Nodal temperature at specific nodes

; NODE_LIST, TEMPER, GROUP

NODE_LIST: node numbers

TEMPER: nodal temperature

GROUP: Load Group Name

*ELTEMPER (Element Temperatures)

Element temperature of specific elements

; ELEM_LIST, TEMPER, GROUP

LEM_LIST: element numbers

TEMPER: element temperature

GROUP: Load Group Name

*BSTEMPER (Beam Section Temperature)

Beam Section Temperature

; ELEM_LIST, DIR, NUM, GROUP             ; line 1

;   TYPE1, ELAST1, THERMAL1, B1, H11, T11, H21,

T21                                                  ; line 2

;   ...

;   TYPEn, ELASTn, THERMALn, Bn, H1n, T1n, H2n, T2n  

           ; line n+1

ELEM_LIST: element numbers

DIR: input direction of beam section temperature load

NUM: number of temperature loads entered

GROUP: Load Group Name

TYPE1: material property to be applied

ELAST1: modulus of elasticity

THERMAL1: thermal expansion coefficient

B1: width to be considered for temperature difference

H11, H21: distance from the centroid to the point of the temperature application

T11, T21: temperatures at H11 & H21

*THERGRAD (Temperature Gradient)

Temperature gradient (difference) between the

upper and lower faces of a beam or plate element

; ELEM_LIST, iETYP, TZ, bUSEHZ, HZ, TY, bUSEHY, HY, GROUP

; ELEM_LIST, iETYP, TZ, bUSEHZ, HZ, GROUP

ELEM_LIST: element number

iETYP: element type {1}

= 1 : beam element

= 2 : plate element

. In the case of beam element

TZ: temperature difference between the two outer faces in the

element local z-direction

bUSEHZ: option to use member dimensions (YES/NO) {YES}

HZ: distance between the two outer faces in the element local z-direction

TY: temperature difference between the two outer faces in the

element local y-direction

 bUSEHY: option to use member dimensions (YES/NO) {YES}

HY: distance between the two outer faces in the element local y-direction

GROUP: Load Group Name.

 In the case of plate element

TZ: temperature difference between the two outer faces in the

element local z-direction

bUSEHZ: option to use member dimensions (YES/NO) {YES}

HZ: thickness of plate element

*WIND (Wind Loads)

Wind loads

; CODE=CODE, SFX, SFY, ESC

                                    ; line 1

; [KS1992]    : EC, BWS, PC                  

                                ; line 2

; [JP1987]    : PRF, WPC

                                                              ; line 2

; [UBC1997]   : EC, BWS, IF, PC

                                                       ; line 2

[ANSI1982]  : EC, BWS, IF, WC, LC

                                                  ; line 2

; [KS2000]    : EC, GF, BWS, IF, HROOF, KZT, HZT

                                                ; line 2

; [IBC2000]   : iPROC, EC, GFX, GFY, BWS, IF, HROOF,

TF, WF, iRIG, iENC, RF        ; line 2

[EURO1992]  : iPROC, RC, RWS, SCC, FORC,

FRIC, TOPO, GRF               ; line 2

; [BS6399(97)]: iPROC, SC, KB, VB, HO, X, CF, SD, TD,

SA, SD, SS, SP, SH               ; line 2

; [CH2001]    : RC, SMT, BWS, MF, WPC, LPC, FPX, FPY

                                 ; line 2

; [JP2000]    : EC, BWS

                                                                   ; line 2

; [NBC1995]   : iPROC, RWS, GEF, CGX, CGY, BH, EC,

bITE, HS, BL, HH, HL, CBD          ; line 2

; SSTORY1, ESTORY1, ADDX1, ADDY1, ...

                                                                        ; from line 3

CODE: select a code to be applied to wind load calculation

= IBC2000, UBC1997, ANSI1982, NBC1995, EURO1992,  BS6399

SFX: scale factor applied to X-direction in GCS

SFY: scale factor applied to Y-direction in GCS

DESC: brief description

 

In the case of [KS1992]

EC: exposure category : 'A', 'B', 'C' {B}

BWS: basic wind speed (unitless) {30}

PC: wind pressure coefficient {1.4}

 

In the case of [JP1987]

PRF: wind pressure reduction factor {0}

WPC: wind pressure coefficient {0}

 

In the case of [UBC1997]

EC: exposure category : 'B', 'C', 'D' {B}

BWS: basic wind speed (unitless) {80mile/h}

IF: importance factor {1}

PC: wind pressure coefficient {1.3}

 

In the case of [ANSI1982]

EC: exposure category: 'A', 'B', 'C', 'D' {A}

BWS: basic wind speed (unitless) {80mile/h}

IF: importance factor {1}

WC: Windward wind pressure coefficient {0.8}

LC: Leeward wind pressure coefficient {0.5}

 

In the case of [KS2000]

EC: exposure category: 'A', 'B', 'C', 'D' {B}

GF: Gust factor

BWS: basic wind speed (unitless) {30}

IR: importance factor

HROOF: average roof height

KZT: wind speed scale factor for topography

HZT: vertical height for wind speed factor

 

In the case of [IBC2000]  

iPROC: calculation method for wind load

= 1: Simplified Procedure

= 2 : Analytical Procedure

EC: exposure category: ‘B’, ‘C’, ‘D’, {B}

GFX: Gust Factor X

GFY: Gust Factor Y

BWS: basic wind speed {30mile/h}

IF: importance factor {1.0}

HROOF: mean roof height

WF: wind directionality factor

iRIG: structural rigidity

= 0 : Rigid Structure

= 1 : Flexible Structure

 

In the case of [EURO1992]

iPROC: calculation method for wind load

= 1: Simplified Method

= 2 : Detailed Method

RC: roughness category: ‘1’, ‘2’, ‘3’, ‘4’, {1}

RWS: reference wind speed {24.5m/sec}

SCC: size coefficient

FORC: force coefficient

FRIC: friction coefficient

TOPO: topography coefficient

GRF: gust response factor

 

In the case of [BS6399(97)

]iPROC: calculation method for wind load

= 1: Standard Method

= 2 : Directional Method

SC: site category (COUNTRY /TOWN)

KB: building type factor {1}

VB: basic wind speed {24m/sec}

HO: mean roof height

X: separation of building

CF: friction drag coefficient

SD: closet diatance to sea

DTdistance to town edge

SA: altitude factor:

SD: directional factor

SS: seasonal factor

SP: probability factor

SH: topographic increment

 

In the case of [CH2001]

RC: roughness category : ‘A’, ‘B’, ‘C’, ‘D’, {A}

SMT: structural meterial type

 = ST: Steel

= SW: Steel + Infilled Wall

= RC: RC

BWS: basic wind pressure

MF: modification factor for

WPC: windward pressure coefficient

LPC: leeward pressure coefficient

FPX: fundamental period of the structure in the X-direction

FPY: fundamental period of the structure in the Y-direction

 

In the case of [JP2000]

EC: exposure category :  ‘¥°’, ‘¥±’, ‘¥²’, ‘¥³’, {¥°}

BWS: basic wind speed {32m/sec}

 

In the case of [NBC1995]

iPROC: calculation method for wind load

= 1: Simple Procedure

= 2 : Detailed Procedure

RWS: reference wind speed {30m/sec}

GEF: Gust factor (Simple Procedure)

CGX: Gust factor (Detailed Procedure)

CGY: Gust factor (Detailed Procedure)

BH: building height

EC: exposure category : ‘A’, ‘B’, ‘C’, {A}

BITE: option to consider the wind speed scale factor according to to

pography {NO}

HS: hill shape

= 2DR : 2-D Ridge or Valley (mountain)

= 2DE : 2-D Escarpment (slope)

= 3DA : 3-D Axisym. Hill (hill)

BL: building location - building location in case 2-D Escarpment

HH: hill height - height of the hill or the difference in elevation between

the crest of the hill and that of the terrain surrounding the upstream

HL: hill length - distance upwind of the crest to where the ground elevation

is half the height of the hill

CBD: crest-building distance

SSTORY1: start story for applying additional wind load

ESTORY1: end story for applying additional wind load

ADDX1: additional wind load in the global X-direction

ADDY1: additional wind load in the global Y-direction

*SEIS (Static Seismic Loads))

Equivalent Static Seismic Loads

; CODE=CODE, SFX, SFY, ECCX, ECCY, DESC

                                    ; line 1

; [KS1992]  : SPT, EA, IF, PAX, PAY, PCX, PCY, RMFX,

RMFY                                  ; line 2

; [UBC1991] : SPT, ZF, IF, PAX, PAY, PCX, PCY, NCX,

NCY                                    ; line 2

; [UBC1997] : SPT, ZF, SST, CD, IF, PX, PY, NCX,

NCY                                    ; line 2

; [ATC306]  : SPC, EPV, PAX, PAY, PCX, PCY, RMFX,

RMFY                                  ; line 2;

[KS2000]  : SPT, EA, IF, PAX, PAY, PCX, PCY, RMFX,

RMFY                                  ; line 2

; [JIS]     : SPT, EA, SF, PAX, PAY, PCX, PCY, RMFX,

RMFY                                  ; line 2

; [IBC2000] : SDC, SC, MS, M1, IF, PX, PY, PCX, PCY, RMFX,

RMFY                                  ; line 2

; [EURO1996]: S, QO, KD, KR, KW, ALPHA, FPX,

FPY                                     ; line 2

; [CH2001]  : NSC, SFI, SC, ST, DR, EQ, bMM, FPX

FPY                                   ; line 2

; [NBC1995] : ZVR, AZ, VZ, IF, FF, PAX, PAY, PCX, PCY,

FMFX, FMFY                     ; line 2

; SSTORY1, ESTORY1, ADDX1, ADDY1, ...

                                       ; from line 3

CODE: select a code to be applied to seismic load calculation

= IBC2000, UBC1997, UBC1991, ATC306, NBC1995, EURO1996

SFX: scale factor applied to X-direction in GCS

SFY: scale factor applied to Y-direction in GCS

ECCX: accidental eccentricity torsion induced by the story  seismic load

in the X-direction in GCS

= POS: counter-clockwise

= NEG: clockwise

ECCY: accidental eccentricity torsion induced by the story  seismic load

in the Y-direction in GCS

= POS: counter-clockwise

= NEG: clockwise

DESC: brief description

 

In the case of [KS1992]

SPT: soil profile type (= 1.0, 1.2, 1.5) {S2(1.2)}

EA: earthquake area factor (= 0.08, 0.12) {Area2(0.12)}

IF: importance factor (= 0.8, 1.0, 1.2, 1.5) {1.2}

PAX: natural period in the X-direction obtained by the eigenvalue analysis {0}

PAY: natural period in the Y-direction obtained by the eigenvalue analysis {0}

PCX: natural period in the X-direction obtained by the code {0}

PCY: natural period in the Y-direction obtained by the code {0}

RMFX: response modification coefficient in X-direction {6}

RMFY: response modification coefficient in Y-direction {6}

 

In the case of [UBC1991]

SPT: soil profile type (= 1.0, 1.2, 1.5) {S1(1.0)}

ZF: seismic zone factor (= 0.075, 0.15, 0.2, 0.3, 0.4) {0.075}

IF: importance factor (= 1.0, 1.25) {1.0}

PAX: natural period in the X-direction obtained by the eigenvalue analysis {0}

PAY: natural period in the Y-direction obtained by the eigenvalue analysis {0}

PCX: natural period in the X-direction obtained by the code {0}

PCY: natural period in the Y-direction obtained by the code {0}

NCX: ductility coefficient : numerical coefficients representative of the

inherent overstrength and global ductility capacity of a lateral force

resisting system in the X-direction

NCY: ductility coefficient : numerical coefficients representative of the

inherent overstrength and global ductility capacity of a lateral force

resisting system in the Y-direction

In the case of [UBC1997]

SPT: soil profile type (= Sa, Sb, Sc, Sd, Se, Sf) {Sa}

ZF: seismic zone factor (= 0.075, 0.15, 0.2, 0.3, 0.4) {0.075}

SST: seismic source type {A}

CD: closest distance to known seismic source {10 KM}

IF: importance factor

PX: natural period in the X-direction obtained by the eigenvalue analysis

PY: natural period in the Y-direction obtained by the eigenvalue analysis

NCX: ductility coefficient : numerical coefficient relative to structural

ductility and over-strength in the X-direction

NCY: ductility coefficient : numerical coefficient relative to structural

ductility and over-strength in the Y-direction

 

In the case of [ATC306]

SPC: soil profile coefficient{0}

EPV: effective peak velocity{0}

PAX: natural period in the X-direction obtained by the eigenvalue analysis {0}

PAY: natural period in the Y-direction obtained by the eigenvalue analysis {0}

PCX: natural period in the X-direction obtained by the code {0}

PCY: natural period in the Y-direction obtained by the code {0}

RMFX: response modification factor in X-direction

RMFY: response modification factor in Y-direction

 

In the case of [KS2000]

SPT: soil profile type (= 1.0, 1.2, 1.5) {S2(1.2)}

EA: earthquake area factor (= 0.07, 0.11) {Area1(0.11)}

IF: importance factor (= 0.8, 1.0, 1.2, 1.5) {1.2}

PAX: natural period in the X-direction obtained by the eigenvalue analysis {0}

PAY: natural period in the Y-direction obtained by the eigenvalue analysis {0}

PCX: natural period in the X-direction obtained by the code {0}

PCY: natural period in the Y-direction obtained by the code {0}

RMFX: response modification coefficient in X-direction {6}

RMFY: response modification coefficient in Y-direction {6}

 

In the case of [JIS]

SPT: soil period {0.6sec (¥±)}

EA:  seismic zone factor

SF: base shear factor

PAX: natural period in the X-direction obtained by the eigenvalue analysis {0}

PAY: natural period in the Y-direction obtained by the eigenvalue analysis {0}

PCX: natural period in the X-direction obtained by the code {0}

PCY: natural period in the Y-direction obtained by the code {0}

RMFX: response modification coefficient in X-direction

RMFY: response modification coefficient in Y-direction

 

In the case of [IBC2000]

SDC: seismic design categories :  ‘A’, ‘B’, ‘C’, ‘D’, ‘E’, ‘F’, {A}

SC: soil class : ‘A’, ‘B’, ‘C’, ‘D’, ‘E’, {A}

MS: mapped spectral response acceleration at short periods {0.25}

M1: mapped spectral response acceleration at 1 second periods {0.1}

IF: Importance factor {1.0}

PX, PY: natural period obtained by eigenvalue analysis

PCX, PCY: natural period obtained by the formula in the code

RMFX, RMFY: response modification coefficient

 

In the case of [EURO1996]

S: soil class {A(1.0)}

QO: basic behavior factor based on structure type {5.0}

KD: ductility class {High (1.00)}

KR: elevation regularity {Regular (1.00)}

KW: failure mode factor {1}

ALPHA: ratio of design ground acceleration to gravity acceleration

FPX, FPY: fundamental period

 

In the case of [CH2001]

NSC: near source category {1}

SFI: seis. fortification intensity {6(0.05g)}

SC: site class {1}

ST: structure type

= RSM: RC or Steel Multistory

=IFM: Interior Framed Multistory

= TSB: Tall Steel Building (JGJ99-98)

= ETC: Etc

DR: damping ratio

EQ: Earthquake frequency

= FREQUENT: frequent earthquake (weak)

= SCARCE: scarce earthquake (strong)

Bmm: whether or not masonry structure type is applied : masonry  

multistory, framed 1st story, interior frame - exterior masonry structure

FPX, FPY: fundamental period

 

In the case of [NBC1995]

ZVR: zonal velocity ratio {0.05}

AZ: acceleration zone : acceleration related seismic zone{1}

IF: importance factor {1}

FF: foundation factor {1}

PAX, PAY: natural period obtained by eigenvalue analysis

PCX, PCY: natural period obtained by the formula in the code

FMFX, FMFY: force modification factor for each direction

 

SSTORY1: start story of additional seismic load to be applied

ESTORY1: end story of additional seismic load to be applied

ADDX1: additional seismic load value in the X-direction in GCS

ADDY1: additional seismic load value in the Y-direction in GCS

*TDN-PRESTRESS (Tendon Prestress Loads)

Apply tendon prestress loads

; TDN-NAME, FORCE/STRESS, JACKING, BEGIN, END,

iGROUTING, GROUP

TDN-NAME: tendon name to which prestress loads are applied

FORCE/STRESS: input tension force in force/stress units

JACKING: order of tentioning tendons

BEGIN: tension force at the start of tendon

END: tension force at the end of tendon

iGROUTING: timing of grrouting duct

GROUP: load group for tendon prestress loads (Load Group Name)

*TIMELOAD (Time Load)

Tme dependent property due to the difference in

member ages

; ELEM_LIST, DAY, GROUP

ELEM_LIST: element numbers subjected to Time Load

DAY: member age

GROUP: Load Group Name

*CREEPCOEF

Creep coefficient directly input in the form of load

; ELEM_LIST, CREEP, GROUP

ELEM_LIST: element numbers for which the creep coefficient is considered

CREEP: creep coefficient

GROUP: Load Group Name

*PNLOADTYPE (Plane Load Type)

Type and size of plane load

; NAME=NAME, TYPE(POINT/LINE/AREA), DESC

; CP_X=X1, X2, ...

; CP_Y=Y1, Y2,

;  DATA=X1, Y1, F1, M1                                            ; T Y P E = P O I N T

;      ...

;      Xn, Yn, Fn, Mn

; DATA=bUNIFORM, TYPE, X1, Y1, L1, X2, Y2, L2                

                        ; TYPE=LINE

; DATA=bUNIFORM, b3PT, X1, Y1, L1, X2, Y2, L2, X3, Y3, L3

X4, Y4, L4                               ; TYPE=AREA

NAME: name of plane load

TYPE(POINT/LINE/AREA): type of load

DESC: brief description

CP_X: copy distance in the x-direction of the plane coordinat

 system for loading simultaneous plane loads

CP_Y: copy distance in the y-direction of the plane coordinate

system for loading simultaneous plane loads

1. In the case of POINT

X1: x-coordinate of the location of loading application

Y1: y-coordinate of the location of loading application

F1: magnitude of the concentrated load

M1: magnitude of the concentrated moment

2. In the case of LINE

bUNIFORM: option to apply a uniformly distributed load

TYPE: assigns the load type

X1, X2: x-coordinate of the entered load

Y1, Y2: y-coordinate of the entered load

L1, L2: magnitude of the entered load

3. In the case of AREA

bUNIFORM: option to apply a uniformly distributed load

 X1, X2, X3, X4: x-coordinate of the entered load

Y1, Y2, Y3, Y4: y-coordinate of the entered load

L1, L2, L3, L4: magnitude of the entered load

*PLANELOAD (Plane Load)

Applying Plane load to any point on plate and solid elements

; LCNAME, LTNAME, ETYPE, GROUP                     

                                 ; 1st line

; ELEM-SEL, ELEM-GROUP, FACE, DIR, PROJ, DESC                 

                         ; 2nd line

; OX, OY, OZ, XX, XY, XZ, YX, YY, YZ, TOL, bLAREA

iNODE1, ... , iNODEn                         ; 3rd line

LCNAME: name of unit load case

LTNAME: name of plane load

ETYPE: type of the selected elements (Plate/Solid)

DIR: direction of the plane load application

bPROJ: option to apply the projectied area

DESC: brief description

GROUP: Load Group Name

OX, OY, OZ: coordinates of the origin point of the plane local coordinate system

XX, XY, XZ: coordinates on the x-axis in the plane local coordinate system

YX, YY, YZ: coordinates on the y-axis in the plane local coordinate system

TOL: coordinate tolerance of a point

bLAREA: select whether or not to assign the loaded area

iNODE1: node numbers defining the outline of plane load

*INIF-CTRL (Initial Force Control Data)

Saving the initial axial force as the results of a separate load case

; bADD, LOADCASE

bADD: option to enter the initial axial force as the results of a

separate load case (YES/NO) {NO}  

LOADCASE: load case, which will save or add initial axial force

*INIFORCE (Initial Forces for Geometric Stiffness )

Entering initial axial forces required to calculate the

geometric stiffness of specific members

; ELEM_LIST, DIR, FORCE

ELEM_LIST: element numbers for which initial axial forces are entered

DIR: direction of initial axial force

 = AXIAL: applies the force as the element’s axial force  

= GX: considers the force in the global X-direction, such that the

axial forces for the object elements are automatically calculated and

entered relative to their orientations  

= GY

 = GZ

FORCE: magnitude of axial force

*SFUNCTION (Specturm Function)

Spectrum data required for response spectrum analysis

; FUNC=NAME, iTYPE, SCALE, GRAV, DESC   ; line 1

; PERIOD1, VALUE1, PERIOD2, VALUE2, ...      ; from line 2

FUNC: name of spectrum data

iTYPE: assigns data type {1}

= 1 : Normalized Acceleration

= 2 : Acceleration

= 3 : Velocity

= 4 : Displacement

SCALE: correction factor for spectrum data {1}

GRAV: gravitational acceleration {9.806 m/sec2

DESC: brief discription

PERIOD1: period value

VALUE1: value of spectrum data

*SPLDCASE (Spectrum Load Cases)

Basic data required for response spectrum analysis

(load case)

; NAME, FUNC, DIR, ANGLE, SCALE, DESC

NAME: name of response spectrum analysis case

FUNC: spectrum function to be applied to response spectrum analyis

DIR: applied direction of spectrum load {XY}     

XY: lateral directions of the structure    

Z: vertical direction of the structure

ANGLE: input angle of seismic load with respect to the X-direction

of GCS if X-Y plane selected

(right hand sign convention about the Z-axis) {0}

SCALE: scale factor for input loads {1}

DESC: brief description

*TFUNCTION (Time History Function)

Time history load function

; FUNC=NAME, 1, iTYPE, SCALE, GRAV, DESC

            ; line 1

; TIME1, VALUE1, TIME2, VALUE2, ...      ; from line 2

; FUNC=NAME, 2, iTYPE, GRAV, A, C, F, D, PA, DESC

NAME: name of time history function

iTYPE: assigns the type of data {1}

= 1 : Normalized Acceleration

= 2 : Acceleration

= 3 : Force

= 4 : Moment

 

For 1 (=Time History Function )

SCALE: the scale factor of data{1}

GRAV: gravitational acceleration {9.806 m/sec2}

DESC: brief discription

TIME1: time

VALUE1: time history load data

 

For 2 (= Sinusoidal Function) {0}

A, C: constantsF:

F:frequency of the input load [Cycle/sec]

D: damping coefficient

PA: phase angle

*THLDCASE (Time History Load Cases)

Basic data required for executing time history analysis

(load case)

; NAME=NAME, DESC                          ; line 1

NAME: name of the load case of the time history function

DESC: brief descriptionn

ETIME: end time of the time history analysis {1sec}

INC: time increment of the time history analysis (0.1 sec)

iOUT: analysis interval required for producing the time history analysis results {1}

iMODE1: mode number {0}

DAMPING1: damping coefficient for each mode {0}

DALL: damping coefficient used for all the modes {0}

*DYN-NLOAD (Dynamic Nodal Loads)

Applying a time history function to nodes in a specific direction

; NODE_LIST, THIS, FUNC, DIR, ARTIME, SCALE

NODE_LIST: node numbers

THIS: selects the time history analysis condition

FUNC: type of time load function

DIR: loading direction of the time load function {X}

= X, Y, Z

ARTIME: arrival (delay) time for the time load function {0sec}

SCALE: scale factor for the time load function {1}

*GROUND-ACC

Specifying a time load function as a ground acceleration

; THIS, FUNCX, SCALEX, ATIMEX, FUNCY, SCALEY,

 ATIMEY, FUNCZ, SCALEZ, ATIMEZ,

THIS: selects the time history analysis condition

 

1. Ground acceleration in the X-direction of the GCS

FUNCX: selected time load function from the list

SCALEX: scale factor for the time load function {1}

ATIMEX: arrival (delay) time for the time load function {0}

 

2. Ground acceleration in the Y-direction of the GCS

FUNCY: selected time load function from the list

SCALEY: scale factor for the time load function {1}

ATIMEY: arrival (delay) time for the time load function {0}

 

3. Ground acceleration in the Z-direction of the GCS

FUNCZ: selected time load function from the list

SCALEZ: scale factor for the time load function {1}

ATIMEZ: arrival (delay) time for the time load function {0}

*DYN-SLOAD (Time Varing Static Load)

Converting static load into time history load

; THIS, SLOAD, FUNC, ATIME, SCALE

THIS: selects the time history analysis condition

SLAOD: Static Load condition

FUNC: name of the Time History Load Function

ATIME: arrival time of the Time History Load Function {0sec}

SCALE: scale factor of the Time History Load Function {1}

 

*TH-GRAPH

Producing time history analysis resuits in graohs relative to time

(displacements, member forces and stresses in truss/beam elements

; NAME, iENTITY, iFTYPE, iSTYPE, iPOS, iCOMP, bALL,

iSEL, iOPT,

1. Common items

NAME: name of the graphic output function of the time

history analysis results

iENTITY: node number of a truss/ beam element

iFTYPE: type of the time history analysis results  to be produced

= 2 : Displacement

= 3 : Truss Force/Stress

= 4 : Beam Force/Stress

 

2. In the case of Displacement

iSTYPE: type of the time history analysis results to be produced in a graph

= 1 : Displ. (displacement)

= 2 : Vel. (velocity)

= 3 : Accel. (acceleration)

iPOS: {1}

iCOMP: direction component of the displacement

= 1 : DX

= 2 : DY

 = 3 : DZ

= 4 : RX

= 5 : RY

= 6 : RZ

bALL: selects the Modes, which will be reflected in the time history calculation

 = YES: All Modes

= NO: One Mode

iSEL: selected Mode

iOPT: {0}

 

3. In the case of Truss Force/Stress

iSTYPE: type of the time history analysis results to be produced

= 1 : Force

= 2 : Stress

iPOS: location on a truss for which the results will be produced

= 1 : I-Node

= 2 : J-Node

iCOMP: member force or stress component

 = 1 : FX    SX

iOPT: {0}

 

4. In the case of Beam Force/Stress

iSTYPE: type of the time history analysis results to be produced

= 1 : Force

= 2 : Stress

iPOS: location on a beam for which the results will be produced

= 1 : I-Node

= 2 : J-Node

iCOMP: member force or stress component

= 1 : Axial                   Axial

= 2 : Shear-y                 Shear-y

= 3 : Shear-z                 Shear-z

= 4 : Torsion                 Bend(+y)

= 5 : Moment-y              Bend(-y)

= 6 : Moment-z              Bend(+z)

iOPT: option to combine Axial  

= 0 : do not consider

= 1 : consider

*LINELANE (Traffic Line Lanes)

Lane data required for applying traffic moving loads

; NAME=NAME, LDIST, GROUP,

                                        ; line 1

; iELEM1, ECC1, FACT1, ...                 ; from line 2

NAME: traffic line lane classification number

LDIST: assign objects to distribute the traffic load

GROUP: Cross Beam Element Group

iELEM1: start element number among the beam element

(or variable section element) numbers

ECC1: eccentricity distance from the center of the beam to the traffic line lane {0}

FACT1: impact factor for the traffic load (0<=FACT<=0.3) {0}

*SURFLANE (Traffic Surface Lanes)

Traffic surface lane data

; NAME=NAME, WIDTH, START, END,

                                                          ; line 1

; iNODE1, OFFSET1, FACT1, ...                ; from line 2

NAME: name of traffic surface lane

WIDTH: width of the traffic lane {0}

START: slope at the starting point

END: slope at the ending point

iNODE1: node numbers defining the traffic surface lane

OFFSET1: distance from iNODE1 to the traffic lane center {0}

FACT1: impact factor for the traffic load (0<=FACT<=3) {0}

*SURFINEL (Plate Elements for Influence Surface)

Entering plate elements for influence surface analysis

; ELEM_LIST

ELEM_LIST: element numbers

*LSUPPORT (Lane Supports )

The supports when calculating the max moment using the

 traffic load ina continuous beam

; ELEM_LIST,

ELEM_LIST: element number

*LSUPPORT2 (Lane Supports ?Reactions at Interior Piers)

Assigning the inner points used in moving load analysis  

; NODE_LIST

NODE_LIST: node numbers of the inner supports

*VEHICLE (Vehicles)

Traffic load

; NAME=NAME, 1

; NAME=NAME, 2,

                                            ; line 1

; LOAD1, DIST1, LOAD1, DIST2, ...        ; from line 2

NAME: name of traffic load

 

For 1:

 Standard Vehicle Load

* refer to the Table below

For 2

: user defines the traffic load traffic load by conbining concentrated

traffic loads and traffic lane loads

 uniformly distributed traffic lane load [force/length] {0}

 concentrated traffic moving load {0}

concentrated traffic moving load used to calculate bending moment {0}

: concentrated traffic moving load used to calculate shear force {0}

LOAD1: concentrated load

DIST1: distance between concentrated loads

 

 

Korean road Standard specification

DB-24, DB-18, DB-13.5,

DL-24, DL-18, DL-13.5

Korean standard train loads

L-25, L-22, L-18, L-15,

S-25, S-22, S-18, S-15,

EL25, EL22, EL18,

HL standard train load,

H15-44, HS15-44, H15-44L, HS15-44L

AASHTO Standard

H20-44,HS20-44, H20-44L, HS20-44L, AML

Caltrans Standard

P5, P7, P9, P11,P13

Other train loads

CE80(Cooper E80 Train Load),

UIC80(UIC80 Train Load)

Table 2. Standard traffic loads

*VCLASS (Vehicle Classes )

Vehicle load group data used for moving load analysis

; NAME=NAME                  ; line 1

VLOAD1, VLOAD2, ...            ; from line 2

NAME: vehicle load group

VLOAD1: vehicle moving load

*MVLDCASE (Moving Load Cases)

Assigning moving load cases using vehicle load groups and traffic lanes

; NAME=NAME, SCALE1, SCALE2, SCALE3, SCALE4,

, DESC                                      ; 1st line

;.VCLASS1, SCALE1, iMIN1, iMAX1, LANE11,

LANE12, ...                          ; 2nd line

; ,.VCLASSn, SCALEn, iMINn, iMAXn, LANEn1

LANEn2, ...                          ; th line

NAME: input the name of moving load condition

SCALE1: reduction factor used for applying multi-traffic lane loads

{1, 1, 0.9, 0.75}

DESC: brief description

VCLASS1: select vehicle load group

SCALE1: scale factor to be applied to traffic load group {1}

iMIN1: minimum number of traffic lanes for loading vehicle load group {1}

iMAX1: maximum number of traffic lanes for loading vehicle load group {1}

LANE11: selected traffic lanes

*SM-GROUP (Settlement Group)

Settlement group

; GRNAME, DISPLACEMENT, NODE_LIST

GRNAME: settlement group name

DISPLACEMENT: size of settlement {0}

NODE_LIST: node number included in the settlement group

*SMLDCASE (Settlement Load Cases )

Support settlement group

Support settlement group

                                                 ; line 1

GRNAME1, GRNAME2, ...             ; from line 2

NAME: name of support  settlement load case

ISMIN:: minimum number of support  settlement groups{1}

ISMAX: maximum number of support  settlement groups{1}

SCALE : scale factor for load{1}

DESC : brief description

GRNAMEL1 : use of selected support  settlement groups

*SEQUENCE-WZD

Defining the formation of elements and  application times of loads in construction stages of a structure

; *SEQUENCE-WZD, LCNAME, DURATION, AGE

;     STEP=NO1, DLSTORY1                   ; line 1

;          iTYPE1, MATL1, MSTORY1, ...     ; from line 2

;     ALOAD=LCNAME     ; from here, additional dead load

;           SDAY1, STORY1, ...

; MATL : ALL, STEEL, CONC, SRC, USER     ; iTYPE=1

; MATL : iMAT                                     ; iTYPE=2

LCNAME: unit load condition applied in the construction stage analysis

DURATION: duration of the construction stage [day]

AGE: initial member age of the element [day]

STEP: construction stage

NO1: sequential number of the construction stage

DLSTORY1: the highest story to which the construction load is applied

iTYPE1: method of defining the element formation in a specific construction stage

= 1: Material Type

= 2: Material Name

1. iTYPE = In case of 1  

MATL1: material applied in the construction load

= ALL

= STEEL

= CONC

= SRC

= USER

2. iTYPE = In case of 2   

MATL1: material number defined

 

ALOAD: applied load

LCNAME: unit load condition applied to the additional load

SDAY1: start time at which the additional load is applied

STORY1: the highest story to which the additonal load is applied

*COMPBOXLC (Load Cases for Pre-composite Section)

Entering pre-composie load case to reflect the change in

section properties of before and after composite

action of a composite structural steel bridge

; LCNAME1, LCNAME2, ..., LCNAMEn

LCNAME1: load case to be used as the pre-composite load

*HYD-PRTEMPER (Prescribed Temperature )

Entering prescribed temperature condition for  Heat of hydration analysis

; NODE_LIST, TEMPERATURE, GROUP

NODE_LIST: nodes subject to a prescribed temperature

TEMPERATURE: Prescribed Temperature

GROUP: Boundary Group

*HYD-PCOOLELEM (Pipe Cooling)

Entering pipe cooling data intended for lowering temperature

; NAME=NAME, DIAMETER, COEF        ; line 1

;      HEAT, DENS, INTEMP, FRATE, iSTART, iEND  

                                                           ; line 2

;      NODE1, NODE2, NODE3, ...              ; from line 3

NAME: pipe cooling group name

DIAMETER: diameter of cooling pipe

COEF: convection coefficient

HEAT: specific heat of water

DENS: density of water

INTEMP: water temperature at the inlet

FRATE: flux per unit time

iSTART: start time of pipe cooling

iEND: end time of pipe cooling

NODE1: nodes defining the course of pipe passage

*HYD-HEATSRCF(Heat Source Function)

Heat source function applied during hydration

; FUNC=NAME, TYPE, TEMPER      ; TYPE=CONST

; FUNC=NAME, TYPE, K, ALPHA     ; TYPE=FUNC

; FUNC=NAME, TYPE, SCALE         ; TYPE=USER (line1)

; TIME1, VALUE1, TIME2, VALUE2, ... ; (from line 2)

1. Common Items

FUNC: name of heat source function

TYPE: type of heat sourse function

= CONST: constant value defined for the heat sourse

= FUNC: code-define heat source function

= USER: user-defined heat source values relative to time in a table form

 

2 In the case of CONST

TEMPER: heat value

 

3. In the case of FUNC

K: maximum adiabatic temperature rise

ALPHA: response speed

 

4. In the case of USER

SCALE: Scale Factor

TIME1: time (hr)

VALUE1: generated heat value

*HYD-CONVCOEF

Change in convection coefficient at the convection

boundary surface of a structure

; FUNC=NAME, TYPE, COEFFICIENT

                                      ; TYPE=CONST

; FUNC=NAME, TYPE, SCALE         

                                      ; TYPE=USER (line 1)

; TIME1, VALUE1, TIME2, VALUE2, ... ; (from line 2)

1. Common Items

FUNC: name of convection coefficient function

TYPE: type of convection coefficient function  

= CONST: convection coefficient defined as a constant value

= USER: user enters the convection coefficients relative to time in a table form

 

2. In the case of CONST

COEFFICIENT: convection coefficient  

 

3. In the case of USER

SCALE: Scale Factor

TIME1: time (hr)

VALUE1: convection coefficient

*HYD-AMBTEMPF (Ambient Temperature Function)

Defining the ambient temperature function to be applied to heat of hydration analysis

; FUNC=NAME, TYPE, TEMPER        ; TYPE=CONST

; FUNC=NAME, TYPE, MAXT, MEANT, DEALY   

                                                      ; TYPE=SINE

; FUNC=NAME, TYPE, SCALE   ; TYPE=USER (line 1)

; TIME1, VALUE1, TIME2, VALUE2, ...  

                                           ; (from line 2)

1. Common Items

FUNC: name of ambient temperature function

TYPE: type of ambient temperature function

= CONST: ambient temperature assigned as a constant value

= SINE: ambient temperature assigned as a Sine function

= USER: user defines the ambient temperature relative to time

 

2. In the case of CONST

TEMPER: ambient temperature

 

3. In the case of SINE

MAXT: max amplitude of ambient temperature

MEANT: temperature immediately after casting

DEALY: delay day immediately after casting

 

4. In the case of USER

SCALE: Scale Factor

TIME1: time(hr)

VALUE1: ambient temperature

*HYD-HEATSRC (Assign Heat Source )

Assigning heat source function to each element (cast concrete)

; ELEM_LIST, FUNCNAME

ELEM_LIST: element numbers to be assigned the heat source function

FUNCNAME: selecting the heat source already entered

*HYD-CONBNDR (Element Convection Boundary)

Entering heat transfer boundary condition due to convection

; ELEM_LIST, CCFUNC, ATFUNC, FACE, GROUP

ELEM_LIST: element numbers to be assigned the convention

boundary condition

CCFUNC: selecting the convection coefficient function already entered

ATFUNC: selecting the ambient temperature function already eneterd

FACE: defining element surfaces after defining the surface number and assigning elements

GROUP: Boundary Group

*HYD-STAGE (Define Construction Stage For Hydration)

Definition of construction stages in order to carry out

the construction stage analysis for the heat of hydration analysis

NAME=NAME                                     ; line 1

;STEP=DAY1, DAY2, ...                           ; line 2

;AELEM=GROUP1, GROUP2, ...               ; line 3

;ABNDR=BGROUP1, BGROUP2, ...           ; line 4

DBNDR=BGROUP1, BGROUP2, ...           ; line 5

NAME: name of the constrction stage to be defined

STEP: elapse time to be defined as Steps within a corresponding construction stage

AELEM: activation of element groups to define active elements within a corresponding construction stage

ABNDR: activation of boundary groups to define active boundart conditions within a corresponding construction stage

DBNDR: defining inactive boundary condition groups

*HINGE-TYPE (Time Dependent Material)

Defining types of plastic hinges for pushover analysis

; NAME=NAME, TYPE

; 1st line (TYPE=AXIAL,MOMENT,SHEAR, PMM)

; NAME=NAME, TYPE, HTYPE, bSYMMETRIC          

 ; 1st line (TYPE=USER)

;      B1P, B2P (, B1N, B2N)  

; 2nd line (TYPE=USER, HTYPE=AXIAL, PMM, TORSION)

;      B1P, B2P, B3P, B4P(, B1N, B2N, B3N, B4N)               

; 2nd line (TYPE=USER, HTYPE=MOMENT, SHEAR)

;      C1P, C2P (, C1N, C2N)                                    

 ; 3rd line (TYPE=USER, HTYPE=AXIAL, PMM, TORSION)

;      C1P, C2P, C3P, C4P (, C1N, C2N, C3N, C4N)               

 ; 3rd line (TYPE=USER, HTYPE=MOMENT, SHEAR)

;      D1P, D2P (, D1N, D2N)                               

 ; 4th line (TYPE=USER, HTYPE=AXIAL, PMM, TORSION)

;      D1P, D2P, D3P, D4P (, D1N, D2N, D3N, D4N)              

 ; 4th line (TYPE=USER, HTYPE=AXIAL, PMM, TORSION)

;      E1P, E2P (, E1N, E2N)   

; 5th line (TYPE=USER, HTYPE=AXIAL, PMM, TORSION)

;      E1P, E2P, E3P, E4P (, E1N, E2N, E3N, E4N)                

; 5th line (TYPE=USER, HTYPE=AXIAL, PMM, TORSION)

;      IOP, LSP, CPP (, ION, LSN, CPN)   

 ; 6th line (TYPE=USER)

;      bUSECALC (, YFP, YFN, YDP, YDN)                       

 ; 7th line (TYPE=USER, HTYPE=AXIAL)

;      bUSECALC (, YMYP, PMYN, YMZP, YMZN, YRYPYRYN, YRZP, YRZN)

7th line (TYPE=USE; R, HTYPE=MOMENT, PMM)

;      bUSECALC (, YFYP, YFYN, YFZP, YFZN, YRYP, YRYN, YRZP, YRZN)         

; 7th line (TYPE=USER, HTYPE=SHEAR)

;      bUSECALC (, YTP, YTN, TRP, YRN)   

; 7th line (TYPE=USER, HTYPE=TORSION)

;      IMETHOD,ALPHA            

 ; 8th line (TYPE=USER, HTYPE=PMM, USECALC=TRUE)

;      IMETHOD, ALPHA, PMAX, bSYMMETRIC                 

 ; 8th line (TYPE=USER, HTYPE=PMM, bUSECALC=FALSE)

;      R01C1, R01C2, R01C3(, R01C4, R01C5)                    

 ; 9th line (TYPE=USER, HTYPE=PMM, bUSECALC=FALSE)

;      ...                                                        ; ...

;      R11C1, R11C2, R11C3 (, R11C4, R11C5)                  

; 19th line  (TYPE=USER, HTYPE=PMM, bUSECALC=FALSE)

1. In the case of AXIAL, MOMENT, SHEAR, PMM

NAME: name of plastic hinge

TYPE: type of plastic hinge

2. In the case of USER  

NAME: name of plastic hinge

TYPE: type of plastic hinge {USER}

HTYPE: user-defined type of plastic hinge

bSYMMETRIC: whether the hinge properties are symmetrical

B, C, D, E: input location of plastic hinge data

P: Positive

N: Negative

IO: Immediate Occupancy

LS: Life Safety

CP: Collapse Prevention

YF: Yield Force

YD: Yield Displacement

YM: Yield Moments

YR: Yield Rotation

YT: Yield Torsion

IMETHOD: apply the Bresler Interpolation method to the P-M interaction diagrams

ALPHA:

 = 1 : linear

 = 2 : elliptic

bUSECALC: whether to automatically calculate the input value of the section data

*HINGE-ASSIGN (Assign Pushover Hinges)

Assigning defined hinge properties to each element

; ELEM_LIST, HINGE_TYPE, LOCATION

ELEM_LIST: element number

HINGE_TYPE: type of assigned hinge

LOCATION: location of the hinge in the element

*INITIAL-LOAD (Initial Load)

Initial load assigned before executing pushover analysis

; LCNAME1, FACT1, LCNAME2, FACT2, ?   : from line

LCNAME1 : unit load condition

FACT1 : load modulus

*POLDCASE (Pushover Load Cases)

Assigning load conditions for pushover analysis

NAME=NAME, DESC                             ; 1st line

;      CTRL_OPT, DISPL                           ; 2nd line

(CTRL_OPT=GLOBAL)

;      CTRL_OPT, MNODE, DIR, DISPL        ; 2nd line

(CTRL_OPT=MNODE)

;      ANAL_OPT, bUSEINILOAD, LOAD_PATTERN    

                                                             ; 3rd line

;      DIR, SCALE                                     ; 4th line

(LOAD_PATTERN=UNIFORM)

;      MODE, SCALE                                 ; 4th line

(LOAD_PATTERN=MODE)

;      LCNAME1, SCALE1, LCNAME2, SCALE2, ...   

                ; from 4th line (LOAD_PATTERN=STATIC)

NAME: name of unit load condition

DESC: brief description

CTRL_OPT: assigning method of the target displacement

1. In the case when the Control Option is GLOBAL

DISPL: max moving displacement

2. In the case when the Control Option is MNODE

MNODE: number for the main node

DIR: direction of the moving displacement

DISPL: max moving displacement

 

ANAL_OPT: conditon of pushover analysis

bUSEINILOAD: assigning method of the initial load

LOAD_PATTERN: assign load type (size ratio)

1. In the case when the Load Pattern is UNIFORM

DIR: direction of the load

SCALE: scale factor

2. In the case when the Load Pattern is MODE

MODE: natural frequency mode

SCALE: scale factor

3. In the case when the Load Pattern is STATIC

LCNAME1: name of the unit load

SCALE1: scale factor

PUSHOVER-CTRL (Pushover Analysis Control Data )

Assign the analysis conditons for pushover analysis

; iMAXINUM, iMAXITER, TOL

iMAXINUM: number of steps to the target displacement

iMAXITER: max iteration

TOL: convergence tolerance

ADDITIONAL-STEP (Additional Steps for Pushover Analysis)

Assign the location of a specific step where the user wishes to check

the results

; STEP1, RATIO1, STEP2, RATIO2, ...      ; from line 1

STEP1: initial step required to determine the location of the additional step

RATIO1: distance ratio from the initial step

*LOAD-SEQ (Loading Sequence)

Assigning the order of applying loads in a

geometrical nonlinear analysis

; LCNAME1, LCNAME2, ...              ; from line 1

LCNAME1: Static Load Cases in the order of application

 

*STAGE (Define Construction Stage )

Defining construction stages to carry out the

construction stage analysis of a bridge

* Where PSC box bridges are analyzed: Wizards, which

automatically define the construction stages, are

 provided for different construction methods such as

ILM,FCM, MSS, etc.

; NAME=NAME, DURATION, bSAVESTAGE

bSAVESTEP                                                    ; line 1

; STEP=DAY1, DAY2, ...                                     ; line 2

; AELEM=GROUP1, AGE1, GROUP2, AGE2, ...     ; line 3

; DELEM=GROUP1, REDIST1, GROUP2, REDIST2, ...  

                                                              ; line 4

; ABNDR=BGROUP1, POS1, BGROUP2, POS2, ...  ; line 5

; DBNDR=BGROUP1, BGROUP2, ...                    ; line 6

; ALOAD=LGROUP1, DAY1, LGROUP2, DAY2, ... ; line 7

; DLOAD=LGROUP1, DAY1, LGROUP2, DAY2, ... ; line 8

NAME: name of the construction stage

DURATION: duration of the construction stage

bSAVESTAGE: analysis results are saved by constrution stages

bSAVESTEP: analysis results are saved by Steps within a construction stage

STEP: elapsed time to be defined as Step within the duration of the

construction stage

AELEM: activation of element groups to define active elements

within a corresponding construction stage

= GROUP1: defining active element groups

= AGE1: member age of the group

DELEM: inactivation of element groups

= GROUP1: defining inactive element groups

= REDIST1: Element Force Reduction, which the percentage of

the internal forces carried by the elements to be deactivated will be

redistributed to the contigous elements

 

ABNDR: activation of boundary groups to define active boundart

conditions within a corresponding construction stage

= BGROUP1: defining active boundary condition groups

= POS1: determining the right positions where a boundary

condition contains restraint conditions or elastic support conditions

= DEFORMED: applying the boundary conditions at the locations

after the strucure has deformed

= ORIGINAL: applying the boundary conditions at the original

locations of the strucural nodes

 

DBNDR: inactivation of boundary group conditions

= BGROUP1: boundary conditon groups to be deactivated

 

ALOAD: activation of load groups to define active load cases

within a corresponding construction stage

= LGROUP1: load groups to be activated

= DAY1: time for activating load groups

 

DLOAD: inactivation of load groups

= LGROUP1: load groups to be deactivated

*LOADCOMB (Combinations )

Load combination conditions to combine the results

of static analysis, moving load analysis,  response spectrum

analysis, time dependent analysis, etc.

; NAME=NAME, KIND, iTYPE, DESC  ; line 1

; ANAL1, LCNAME1, FACT1, ...              ; from line 2

NAME: name of load combination condition

= gLCB: General LCB

= cLCB: Concrete LCB

= sLCB: Steel LCB

= rLCB: SRC LCB

= fLCB: Footing LCB    

KIND: type of load combination

= GEN: General= STEEL: Steel Design

= CONC: Concrete Design

= SRC: SRC Design

= FDN: Footing Design

iTYPE: type of load combination method {0}

= 0 : Linear

= 1 : +SRSS

= 2 : -SRSS

DESC: brief ciscription

ANAL1: type of load case

= ST: Static

= RS: Response Spectrum

= TH: Time History

= MV: Moving

= SM: Settlement

LCNAME1: names of load cases

FACT1: load factors to be applied to load cases {1}

*ANAL-CTRL

Number of maximum iterations and

convergence tolerance when analysis is

performed using nonlinear elements and the

basic boundary conditions of individual elements in a structure

bARDC: auto rotational DOF constratint for truss/plane stress/solid elements(YES/NO)

bANRC:auto normal rotation constraint for plate elements(YES/NO)

iTYPE: type of analysis method when performing an analysis using nonlinear elements

= 0 : when performing a repetetive analysis, stiffness of inactive members is included.

= 1 : when performing a repetetive analysis, stiffness of inactive members is excluded.

iITER: maximum number of iterations when performing an

analysis using nonlinear elements

TOL: convergence tolerance when performing an analysis using nonlinear elements

iSITER: number of iterations for which loads are used to check the convergence  

condition in each repetitive analysis stemming from changing stiffness of

the structure for each load case

*PDEL-CTRL (P-Delta Analysis Control )

Load cases and control for iteration required for

carrying out buckling analysis of a structure

; iITER, TOL                                                  ; line 1

; LCNAME1, FACT1, LCNAME2, FACT2, ...        ; from line 2

iITER: number of iterations for P-Delta analysis {5}

TOL: convergence tolerance{1e-5}

LCNAME1: name of load case

FACT1: load factor {1}

*BUCK-CTRL (Buckling Analysis Control)

Load cases and related data required for carrying

out buckling analysis of a structure

; iMODENUM, iITER, TOL                               ; line 1

; LCNAME1, FACT1, LCNAME2, FACT2, ...        ; from line 2

iMODENUM: number of buckling modes {0}

iITER: number of iterations required for the process of Subspace

 Iteration in a buckling analysis {30}

TOL: convergence tolerance{1e-6}

LCNAME1: casename of load

FACT1: load factor {1}

*EIGEN-CTRL (Eigenvalue Analysis Control )

Control data for eigenvalue analysis

iFREQ: requencinumber of natural fes for the structure {0}

iITER: number of iterations required for eigenvalue analysis {20

}iDIM: size of Subspace {0}

TOL: convergence tolerance {1e-6}

bINCNI: include NL-link force vectors(YES/NO) {NO}

iGNUM: number of generations for each NL-link force vectors

*SPEC-CTRL (Response Spectrum Analysis Control)

Combination method of modes in a response spectrum analysis

; TYPE, DAMPING, bADDSIGN

TYPE: method of combining modes in a response spectrum analysis

= SRSS, CQC, ABS {SRSS}

DAMPING: damping ratio

bADDSIGN: whether to revive signs in the analysis results

= YES: use of (+), (-) when combining modes

= NO: do not use signs

*MOVE-CTRL (Moving Load Analysis Control)

Analysis method and output locations of element

results in a moving load analysis

; METHOD, POINT,  PLATE, , FRAME,

,.bREAC, bRG, RGN, bDISP, bDG, DGN, bFM, bFG, FGN

METHOD: method of moving load analysis {1}

= 1 : Exact

= 2 : Pivot

= 3 : Quick

POINT: point of vehicle load application

PLATE: calculation of member forces of plate elements per unit length {1}

= CENTER: calculation of member force per unit length relative to

the center point of the element

= NODAL: calculation of member force per unit length relative to

the center point of the element and the nodes composing the element

Frame: member force output at 5 Points for Frame elements

=NORMAL: member forces at 5 Points for beam elements

=Axial: calculating the member forces at 5 Points, max/min axial

force and moments are calculated and produced

bREAC: option to output the reaction values when producing the

output for moving load analysis results for a reaction (YES/NO) {YES}

bRG: option to assign groups when producing output for reaction values (YES/NO) {NO}

RGN: name of the assigned group when producing output for reaction values

bDISP: option to output the displacement values when producing

the output for moving load analysis results for a displacement

(YES/NO) {YES}

bDG: option to assign groups when producing output for

displacement values (YES/NO) {NO}

DGN: name of the assigned group when producing output for

displacement values

bFM: option to output the member force values when producing the

 output for moving load analysis results for a member force (YES/NO) {YES

bFG: option to assign groups when producing output for

member force values (YES/NO) {NO}

FGN: name of the assigned group when producing output for

member force values

*HYD-CTRL (Hydration Analysis Control )

Aalysis conditions required for heat of hydration analysis

; bLAST-FINAL, STAGE, CN-FACTOR, INIT-TEMPER, EVALUATION, bCNS, TYPE, iITER, TOL

bLAST-FINAL: selection of a construction stage, which is  

considered as the Final stage of the structure during the

construction-staged heat of hydration analysis

= YES: Last Stage

= NO: Other Stage

STAGE: construction stage to be applied as the final stage

CN-FACTOR: Temporal Discretization Factor in heat transfer analysis

INIT-TEMPER: initial temperature used in heat transfer analysis

EVALUATION: location of a solid element for which stresses are produced

= CENTER: stess in the center point of the solid element used as the stess in the

entire element

= GAUSS: Gauss integration point stresses used as the nodal stresses

= NODAL: interpolated nodal stresses using the Gauss integration point stresses

bCNS: option to reflect the effects or creep and shrinkage

(YES/NO) {NO}

TYPE: select ion of creep and shrinkage

= CREEP: consider only creep

= SHRINK: consider only shrinkage

= BOTH: consider both creep and shrinkage

iITER: max number of iterations for an analysis reflecting creep

TOL: convergence tolerance

*NONL-CTRL (Nonlinear Analysis Control )

Assignment of analysis conditions required for a

nonlinear analysis considering large displacements

; ITER, LSTEP, MAX, bENGR, EV, bDISP, DV, bFORC, FV

                                                 ; ITER=NEWTON

; ITER, IFR, MINC, MITER, MDISP bENGR, EV, bDISP, DV,

bFORC, FV                                  ; ITER=ARC

1. In the case of Newton-Raphson

ITER: selection of the method of iterative analysis

= NEWTON: Newton-Raphson

= ARC: Arc-Length

LSTEP: total load divided into the number of Load Steps and applied to each step.

MAX: maximum number of iterations of analysis for each Load Step

bENGR: assement of convergence by Norm base value of energy

(load ¢¥displacement) (YES/NO) {NO}

EV: energy Norm

bDISP: assement of convergence by Norm base value of

 displacement (YES/NO) {NO}

DV: displacement Norm

bFORC: assement of convergence by Norm base value of  

member force

(YES/NO) {NO}  

FV: member force Norm

 

2. In the case of Arc-Length

IFR: Ratio of the Initial Force for Unit Arc-Length

MINC: maximum number of increment steps

MITER: maximum number of iterations of analysis for each Increment Step

MDISP: magnitude of maximum displacement

*STAGE-CTRL (Construction Stage Analysis Control Data )

Assignment of analysis conditions required for using

the analysis functions for a bridge by construction stages

; bLAST-FINAL, FINAL-STAGE,

                                                            ; line 1

; bINC-NLA, iMAXITER, bENEG, EV, bDISP, DV, bFORC,

FV                                                         ; line 2

; bINC-TDE, bCNS, TYPE, iITER, TOL,

                                                ; line 3

; bOUCC, bITS, iITS, bATS, iT10, iT100, iT1K, iT5K, iT10K

                                                             ; line 4

bLAST-FINAL: selection of a construction stage, which is  considered

as the Final stage of the structure during the construction stage analysis

= YES: Last Stage

= NO: Other Stage

FINAL-STAGE: construction stage to be applied as the final stage

bINC-NLA: option to include nonlinear analysis reflecting the

change of geometric shapes (YES/NO) {NO}  

iMAXITER: max number of iterative analyses for each Load Step

bENEG: assement of convergence by Norm base value of

energy (load ¢¥displacement)  (YES/NO) {NO}

EV: energy Norm

bDISP: assement of convergence by Norm base value of  

displacement (YES/NO) {NO}

DV: displacement Norm

bFORC: assement of convergence by Norm base value of  

member force (YES/NO) {NO}  

FV: member force Norm

bINC-TDE: option to analyze the structure by reflecting the time

dependent material properties (YES/NO) {NO}

bCNS: option to consider creep and shrinkage (YES/NO) {NO}  

TYPE: select ion of creep and shrinkage  

= CREEP: consider only creep  

= SHRINK: consider only shrinkage  

= BOTH: consider both creep and shrinkage

iITER: max number of iterations when performing an analysis reflecting creep

TOL: convergence tolerance

: option to consider creep and shrinkage when

reflecting the tension force loss in tendons (YES/NO) {NO}  

: option to apply the change of modulus of elasticity of

concrete based on member ages (YES/NO) {NO}  

: option to consider elastic shortening when reflecting

the tension force loss in tendons (YES/NO) {NO}

bOUCC: only the user-specified creep coefficient used (YES/NO) {NO}

bITS: option to create Additional Step when considering creep (YES/NO)

iITS: number of Time Steps to be created internally

bATS: option to automatically create Time step when T (Time Gap) is large (YES/NO)

iT10: number of Time steps to be created when T>10

iT100: number of Time steps to be created when T>100

iT1K: number of Time steps to be created when T>1000

iT5K: number of Time steps to be created when T>5000iT10K: number of Time steps to be created when T>10000

*DGN-MATL (Modify Steel (Concrete) Material)

Used when changing input material data or when

modifying the material data of concrete and steel

; iMAT, TYPE, MNAME, [DATA1]              ; STEEL

; iMAT, TYPE, MNAME, [DATA2], RBCODE, RBMAIN

RBSUB, FCI ; CONC

; iMAT, TYPE, MNAME, [DATA3], [DATA4], RBCODE

RBMAIN                                                 ; SRC

; [DATA1] : 1, DB, NAME or 2, ELAST, POISN, DEN, FU,

FY1, FY2, FY3, FY4

; [DATA2] : 1, DB, NAME or 2, ELAST, POISN, DEN, FC

; [DATA3] : 1, DB, NAME or 2, ELAST, FU, FY1, FY2, FY3, FY4

; [DATA4] : 1, DB, NAME or 2, ELAST, FC

iMAT: material number

TYPE: type of material  

= CONC

= STEEL

= SRC

MNAME: name of material

RBCODE: select a standard for reinforcing steel

 = KS (RC)

= KS-Civil (RC)

RBMAIN: material of the main reinforcing steel

= SD 24

= SD 30

= SD35

= SD40

RBSUB: material of the beam reinforcing steel (shear steel)

= SD 24

= SD 30

= SD35

= SD40

In the case of [DATA1]

1 = DB: Database (*refer to MATERIAL)    

NAME: name of the database

2 = ELAST: modulus of elasticity    

POISN: poisson’s ratio     

DEN: density    

FU: Tensile Strength    

FY1~FY4: Yield strenths for different thicknesses of members

based on applicable standard

In the case of [DATA2]

2 = ELAST: elastic modulus of concrete    

POISN: poisson’s ratio of concrete

DEN: density of concrete     

FC: design standard strength of concrete

*DGN-SECT

Printing out forces of plate elements in a graph form at a selected cutting line

; iSEC, TYPE, SNAME, OFFSET, SHAPE, [DATA]

{, CCSHAPE}                                  ; DB/USER

; iSEC, TYPE, SNAME, OFFSET, SHAPE, BLT, D1, D2, D3,

D4, D5, D6                                      ; 1st line - VALUE

;       AREA, ASy, ASz, Ixx, Iyy, Izz      ; 2nd line

;       CyP, CyM, CzP, CzM, QyB, QzB, PERI_OUT, PERI_IN

Cy, Cz                                            ; 3rd line

; iSEC, TYPE, SNAME, OFFSET, SHAPE, iREPLACE

ELAST, DEN, POIS, POIC                 ; 1st line - SRC

;       D1, D2, [DATA]                      ; 2nd line

; iSEC, TYPE, SNAME, OFFSET, SHAPE, 1, DB, NAME1,

NAME2, D1, D2                       ; COMBINED

; iSEC, TYPE, SNAME, OFFSET, SHAPE, 2, D11, D12, D13,

D14, D15, D21, D22, D23, D24

; iSEC, TYPE, SNAME, OFFSET, SHAPE, iyVAR, izVAR

STYPE                               ; 1st line - TAPERED

;       DB, NAME1, NAME2         ; 2nd line (STYPE=DB)

;       [DIM1], [DIM2]          ; 2nd line (STYPE=USER)

;       D11, D12, D13, D14, D15, D16                             ; 2nd

line (STYPE=VALUE)

;       AREA1, ASy1, ASz1, Ixx1, Iyy1,

Izz1                             ; 3rd line (STYPE=VALUE)

;       CyP1, CyM1, CzP1, CzM1, QyB1, QzB1, PERI_OUT1

PERI_IN1, Cy1, Cz1             ; 4th line(STYPE=VALUE)

;       D21, D22, D23, D24, D25, D26                             ; 5th

line (STYPE=VALUE)

;       AREA2, ASy2, ASz2, Ixx2, Iyy2,

Izz2                             ; 6th line (STYPE=VALUE)

;       CyP2, CyM2, CzP2, CzM2, QyB2, QzB2, PERI_OUT2,

PERI_IN2, Cy2, Cz2             ; 7th line (STYPE=VALUE)

; [DATA] : 1, DB, NAME or 2, D1, D2, D3, D4, D5, D6

; [DIM1], [DIM2] : D1, D2, D3, D4, D5, D6

* refer to Section

*DGN-CTRL (General Design Data)

Input required data for design

; bFRAMEX, bFRAMEY, bAUTOKF

                     ; 1st line

; STORY1, XMIN1, XMAX1, YMIN1, YMAX1, RMIN1,

RMAX1                                                 ; 2nd line

; ...                                                         ; ...

; STORYn, XMINn, XMAXn, YMINn, YMAXn, RMINn

RMAXn                                                 ; n+1th line

bFRAMEX: define Unbraced | Sway or Braced | Non-sway frame in the global X-direction.

bFRAMEY: define Unbraced | Sway or Braced | Non-sway frame in the global Y-direction.

bAUTOKF: select if the effective buckling length factors are to be automatically calculate.d

LC1: the live load cases that the live load reduction factor is applicable

RT: the methods for calculating the live reduction factor

 0 = General Design Code

 1 = Chinese Standard

DT: design type

3D: 3-D

XY: X-Y plane

XZ: X-Z plane

YZ: Y-Z plane

bAF: live load reduction factor of axial force(YES/NO)

bMO: live load reduction factor of moments(YES/NO)

bSF: live load reduction factor of shear force(YES/NO)

STORY1: name of the reference story where the live load reduction factor is to be applied

XMIN1, XMAX1: the minimum(maximum) global X-coordinate

YMIN1, YMAX1: the minimum(maximum) global Y-coordinate

RMIN1, RMAX1: The range within which the live load reduction factor is to be applied

*DGN-STEEL (Steel Design Code)

Select the design code to apply for the strength verification of steel members and specify the lateral bracing condition of the structure's horizontal members (beams and girders

; CODE, bBRACED, bSPSEIS, iCLASS

CODE: Steel design code { AISC-LRFD93 }

= AISC-LRFD 2k & 93

= AISC-ASD89

= BS5950-90

= Eurocode3

= CSA-S16-01

= AISI-CFSD86

bBRACED: Specify the lateral brace condition to the horizontal members (beams and girders) of the structure to be designed (YES/NO){NO}

bSPSEIS: whether to apply the Special Provisions for Seismic Design according to GBJ17-88 Code

iCLASS: earthquake resistance grade when the Special Provisions for Seismic Design according to GBJ17-88 Code

= 0: Grade -1

= 1: Grade-2

= 2: Grade-3

= 3: Grade-4

safety grade of the structure when not applied

= 0: Level 1 (Strategic)

= 1: Level 2 (Primary)

= 2: Level 3 (Secondary)

*DGN-CONC (Concrete Design Code)

Determine the applicable design code and the applicability of special provisions for seismic design for the design of or the strength verification for RC members

; CODE, bSPECIAL, PHI-B, PHI-T, PHI-C1, PHI-C2, PHI-V,

RHOW, RHOC, RHOR, KIND                  ; line 1

; TLF, SLF                                             ; line 2

; COMB1, COMB2, COMB3, ...

CODE: RC design code { ACI318-02 }

= ACI318-02/99/95/89

= CSA-A23.3-94

= BS8110-97

= Eurocode2

bSPECIAL: Option to apply the special provisions for seismic design (YES/NO){NO}

PHI-B: Strength reduction factor for pure flexure or flexure + axial tension {0.85}

PHI-T: Strength reduction factor for axial tension {0.85}

PHI-C1: Strength reduction factor for spirally reinforced columns subjected

to axial compression or flexure + axial compression {0.75}

PHI-C2: Strength reduction factor for tied columns subjected to axial compression or flexure + axial compression {0.7}

PHI-V: Strength reduction factor for shear {0.8}

RHOW: Limiting maximum rebar ratio for shear wall members {0.04}

RHOC: Limiting maximum rebar ratio for column members {0.03}

RHOR: Limiting maximum rebar ratio for brace members {0.03}

KIND: design methods for Column and Brace according to AIJ-WSD99 Code

0 = method 1 (by N+My, N+Mz)

1 = method 2 (by fixed N, combined My, Mz)

2 = method 3 (by rotated Neutral Axis)

*DGN-SRC (SRC Design Code)

Enter the design code applicable for strength verification of SRC (Steel-Reinforced Concrete composite) members

; CODE, iMATERIAL, bSPSEIC, iCLASS

CODE: SRC design code {SSRC79}

IMATERIAL: material type

= 0 : SRC

bSPSEIC: whether to apply the Special Provisions for Seismic Design according to JGJ138-01 Code

iCLASS: whether to apply the Special Provisions for Seismic Design according to JGJ138-01 Code

= 0: Grade-1

= 1: Grade-2

= 2: Grade-3

= 3: Grade-4

safety grade of the structure when not applied

= 0: Level 1 (Strategic)

= 1: Level 2 (Primary)

= 2: Level 3 (Secondary)

*CB-FACTOR (Bending Coefficient)

Bending Coefficient required for calculating the allowable bending stress or the design strength of the compression flange subjected to the bending moment about the strong axis (y-axis)

; ELEM_LIST, bAUTOCALC, CB

ELEM_LIST: element number

bAUTOCALC: apply this item if the value is to be auto-calculated by the program  (YES/NO){NO}

CB: bending coefficient {1}

*CM-FACTOR (Moment Factor)

the Equivalent Moment correction Factor of the beam-column members

; ELEM_LIST, bAUTOCALC, CMy, CMz

ELEM_LIST: element number

bAUTOCALC: apply this item if the value is to be auto-calculated by the program  

(YES/NO){NO}

CMy: Equivalent moment correction factor applied to the unbraced length portion of a member bent about its strong axis {0}

CMz: Equivalent moment correction factor applied to the unbraced length portion of a member bent about its weak axis {0}

*CV-FACTOR (Shear Coefficient)

Shear coefficient

; ELEM_LIST, bAUTOCALC, CV

ELEM_LIST: element number

bAUTOCALC: apply this item if the value is to be auto-calculated by the program  (YES/NO){NO}

CV: shear coefficient

*DFN-ALLOWABLE (SpecifyAllowable Stress)

Enter the allowable stress coefficients if user may wish to define the

allowable stresses

; ELEM_LIST, FA, FT, FBy, FBz, FV

ELEM_LIST : element number

FA: Allowable compression stress coefficient for the compressive force along the member's axial direction {0.5}

FT: Allowable tension stress coefficient for the tensile force along the member's axial direction {0.6}

FBy: Allowable bending stress coefficient for the bending moment about the member's strong axis {0.6}

FBz: Allowable bending stress coefficient for the bending moment about the member's weak axis {0.6}

FV: Allowable shear stress coefficient for the shear force {0.4}

*F-MAGNIFY (Moment Magnifier)

Moment Magnification Factors

; ELEM_LIST, B1y, B1z, B2y, B2z

ELEM_LIST : element number

B1y: Moment magnification factor for members subjected to vertical loads in a frame braced against sidesway for strong axis bending {0}

B1z: Moment magnification factor for members subjected to vertical loads in a frame braced against sidesway for weak axis bending {0}

B2y: Moment magnification factor for members subjected to horizontal loads in a frame unbraced against sidesway for strong axis bending {1}

B2z: : Moment magnification factor for members subjected to horizontal loads in a frame unbraced against sidesway for weak axis bending. {1}

*K-FACTOR (Effective Length Factor)

Effective Length Factors for the unbraced lengths

; ELEM_LIST, Ky, Kz

ELEM_LIST: element number

Ky: Effective buckling length factor for buckling about strong axis {1}

Kz: Effective buckling length factor for buckling about weak axis {1}

*LENGTH (Unbraced Length)

the unbraced lengths for buckling about the strong (y-axis) and weak (z-axis) axes of the selected compression membersthe laterally unbraced length for the compression flange of a member bent about its weak axis

; ELEM_LIST, Ly, Lz, bNOTUSE, Lb, bAUTOCALC, Le

ELEM_LIST : element number

Ly: Unbraced length for buckling about strong axis (determined by braces in z-dir.)

Lz: Unbraced length for buckling about weak axis (determined by braces in y-dir.)

bNOTUSE: Select this item, if the allowable bending stress computation about the member`s strong axis is to neglect the laterally unbraced length (YES/NO){NO}

Lb: Laterally unbraced length

bAUTOCALC: Select this item, if the Effective Unbraced Length, Le is auto-calculated according to the BS 5950-90 Code

Le: the Effective Unbracedl Lngth according to the BS 5950-90 Code

*REDUCTION ( Modify Live Load Reduction Factor)

Reduction factor of the live loads acting on the relevant columns, shear

walls or footings when calculating the required axial strength

; ELEM_LIST, FACTOR

ELEM_LIST: element number

FACTOR: Live load reduction factor {1}

*MEMBERTYPE (ModifyMember Type)

The type of members used in the design of steel and RC members

; ELEM_LIST, TYPE

ELEM_LIST: element number

TYPE: the member type to be used in design

= Beam

= Column

= Brace

*STIFFENER (Longitudinal Stiffener of Box Section)

The spacings and size of transversal/longitudinal stiffeners for box sections

; iSEC, ASTF, BSTF, TSTF, iNOy, iNOz

iSEC: Section property number for the box member for which the strength is be verified

ASTF: Spacing of the transverse stiffeners

BSTF: Width of the longitudinal stiffener

TSTF: Thickness of the longitudinal stiffener

iNOy: Number of panels on the flange side separated by the longitudinal stiffeners {2}

iNOz: Number of panels on the web side separated by the longitudinal stiffeners {2}

*LIMITSRATIO (Limit Slenderness Ratio  )

Allowable limit slenderness ratio

; ELEM_LIST, bNOTCHECK, COMP, TENS

ELEM_LIST: element number

NOTCHECK: Select this item if the limiting slenderness ratios (KL/r)

are of no interest. If selected, design results reflecting the slenderness effects are

not produced. (YES/NO){NO}

COMP: Limiting slenderness ratio for members under axial compression {200}

TENS: Limiting slenderness ratio for members under axial tension {300}

*DGNCRITERIA (Design Criteria of Rebar)

Enter the standard sizes of main and sub-rebars used in the design of beam, column and brace members.Also, enter the standard sizes and spacing for vertical and horizontal rebars used in the design of shear wall members.

; STIR, SIDE, DT, DB, MAIN1, MAIN2, MAIN3, MAIN4

MAIN5, iSRBN                                ; line 1 - beam

; STIR, DO, MAIN1, MAIN2, MAIN3, MAIN4, MAIN5

iSRBN                                           ; line 2 - column

; STIR, DO, MAIN1, MAIN2, MAIN3, MAIN4, MAIN5

iSRBN                                           ; line 3 - brace

; END, HORZ, DE, DW, VERT1, VERT2, VERT3, VERT4,

VERT5                                          ; line 4 - wall

; DIST1, DIST2, DIST3, iMETHOD, bBEND

                                                    ; line 5 - spacing1

; HORZ, VERT1, VERT2, VERT3, ..., VERT50             

                                                    ; line 6 - spacing2

1.  For Beam Design

STIR: Standard sizes for transverse reinforcing bars in beam design {D10}

SIDE: Standard sizes for side bars, used for bar placing. Beam strength is not affected {D13}

DT: Distance between the center of the main rebars in the top layer of the top bars and the top surface of the section {0}

DB: Distance between the center of the main rebars in the lower layer of the bottom bars and the bottom surface of the section {0}

MAIN1: Main rebar standard sizes for the design of beam members {D22}

iSRBN: Number of shear reinforcement legs

2. For Column Design

STIR: Standard sizes for tie bars used in column design {D10}

DO: Distance between the center of the main rebars and the perimeter surface of the section {0}

MAIN1: Main rebar standard sizes for the design of column members {D22}

iSRBN: the number of layers in the stirrup rebars

3. For Brace Design

STIR: Standard sizes for tie bars used in brace design {D10}

DO: Distance between the center of the main rebars and the perimeter surface of the section {0}

MAIN1: Main rebar standard sizes for the design of brace members {D22}

* If d0 is not entered (ie. 0), the program uses the larger of 2.5?(63.5mm) and H/10, but not exceeding 3 inches

4. For Shear Wall Design

END: The minimum standard size to be used for end rebars for shear wall design {D10}

HORZ: Standard size for horizontal rebars used in shear wall design {D10}

DE: Distance from the end of the shear wall member to the center of the first row of the vertical rebars (or end rebars) {0}

DW: Distance between the center of the end vertical rebars and the end of the shear wall {0}

VERT1: Standard sizes for vertical rebars used in shear wall design {D13}

Spacing1

DIST1: Spacing of end rebars in the case of 4 end rebars {0.3M}

DIST2: Spacing of end rebars in the case of 6 end rebars {0.15M}

DIST3: Spacing of end rebars in the case of 8 end rebars {0.1M}

iMETHOD: The method of designing shear walls considering end rebars {1}

= 1: Method-1

= 2: Method-2

= 3: Method-3

= 4: Method-4

bBEND: Determine whether to design the wall for a bending moment about the weak axis (YES/NO){NO}

Spacing2

HORZ: Spacing of horizonal rebars {0}

VERT1: Spacing of vertical rebars {0}

* If the values dw and de are not entered (in case where they are 0), 2 inches (5.08cm) are automatically used.

*REBAR-BEAM (Modify Beam Section Data)

Enter the section dimensions and rebar data for RC beam members for strength verification

; iSEC, SBARNAME, DT, DB                                ; line1

; iTIARR, iTIRB1, iTIRB2, TINAME, iBIARR, iBIRB1

iBIRB2, BINAME, ISPACE, iISRBN                        ; line 2

; iTMARR, iTMRB1, iTMRB2, TMNAME, iBMARR,

iBMRB1, iBMRB2, BMNAME, MSPACE, iMSRBN   ; line 3

; iTJARR, iTJRB1, iTJRB2, TJNAME, iBJARR, iBJRB1,

iBJRB2, BJNAME, JSPACE, iJSRBN                       ; line 4

iSEC: property number of the beam members

SBARNAME : Standard sizes of the stirrup rebar

DT: Distance between the center of the top main rebars in the upper layer and the top surface of the section {0}

DB: Distance between the center of the bottom main rebars in the lower layer and the bottom surface of the section {0}

iTIARR: Top rebar data at node i of the beam members {1}

= 1: one layer

= 2: two layers

iTIARB1: Number of top rebars in the upper layer at node i

iTIARB2: Number of top rebars in the lower layer at node i

TINAME: Standard sizes of the top rebar

iBIARR: Bottom rebar data at node i of the beam members {1}

= 1: one layer

= 2: two layers

iBIRB1: Number of bottom rebars in the upper layer at node i

iBIRB2: Number of bottom rebars in the lower layer at node i

BINAME: Standard sizes of the bottom rebar

ISPACE: Spacing of stirrup bars

iISRBN: the number of layers of the stirrup rebars in the i node section

* line3 and line4 each shows the rebar information of the  Middle, J end.  The form is the same as line2, so therefore omitted

* when using the initial value ??as the cover thickness, the value automatically calculated within the program will be used in the element design and strength inspection

*REBAR-COLUMN (Modify Column Section Data)

Enter the section dimensions and rebar data for RC column members for strength verification.

; iSEC, HOOP, RBNAME, iNQRB, iNROW, DO, SRBNAME, SPACE, iSRBN

iSEC: property number of the column members

HOOP : the type of hoop rebars {Tied}

= TIED

= SPIRAL

RBNAME: Standard sizes of the main rebar

iNQRB: Number of vertical rebars placed in the column section

iNROW: Number of rows of vertical rebars placed in the column section

DO: Distance between the center of the main rebars and the perimeter surface of the section {0}

SRBNAME: Standard sizes of the hoop rebar

SPACE: Spacing of hoop rebars

iSRBN: the number of layers in the stirrup rebars in the arrangement section

* when using the initial value ??as the cover thickness, the value automatically calculated within the program will be used in the element design and strength inspection.

*REBAR-BRACE (Modify Brace Section Data)

Enter the section dimensions and rebar data for RC brace members for strength verification

; iSEC, HOOP, RBNAME, iNQRB, iNROW, DO, SRBNAME, SPACE, iSRBN

iSEC: property number of the brace members

HOOP: the type of hoop rebars {Tied}

= TIED

= SPIRAL

RBNAME: Standard sizes of the main rebar

iNQRB: Number of vertical rebars placed in the brace section

iNROW: Number of rows of vertical rebars placed in the brace section

DO: Distance between the center of the main rebars and the surface of the section {0}

SRBNAME: Standard sizes of the hoop rebar

SPACE: Spacing of hoop rebars

ISRBN: the number of layers in the stirrup rebars in the arrangement section

* when using the initial value ??as the cover thickness, the value automatically calculated within the program will be used in the element design and strength inspection.

*REBAR-SRC (Modify SRC Section Data)

Enter the rebar data and SRC section data required to perform strength verification of Steel-Reinforced Concrete Composite Columns.

; iSEC, bCALC, SPACE, RBNAME, iNQRB, iNROW, DO, SRBNAME, SSPACE

iSEC: Section property number for which the SRC members

bCALC: Select the option if the spacing of main rebars is to be auto-calculated in the program. (YES/NO){NO}

SPACE: spacing of the main rebars

RBNAME: the standard size of the main rebars

iNQRB: the number of the main rebars

iNROW: Number of main rebar rows in the SRC section.

DO: Distance (cover thickness) from the center of the main rebars to the face of the concrete section {0}

SRBNAME: Standard sizes of the stirrup rebar

SSPACE: Spacing of stirrup rebars

* Enter the cover thickness of the main rebars in the SRC section. If the cover thickness is not entered for the main rebars (do = 0), the program calculates as follows :

do = MAX (Hc/10, Bc/10, 2.5) in ¡Â 3 in

*REBAR-WALL (Modify Wall Section Data)

Enter the design criteria for shear wall members- the standard rebar sizes, the rebar placement, the number of rebars, the thickness of the shear wall section, etc., for the stories assigned by the user for strength verification.

; iWID, STORY, bMODELTHK, THIK, VRBNAME, VRBSPACE, ERBNAME, ERBSPACE, iERBNUM, HRBNAME, HRBSPACE, DW, DE

iWID: Shear wall ID number

STORY: The story Names from which the design data are applicable

bMODELTHK: Select the option if the thickness of the shear wall member is to be applied. (YES/NO){NO}

THIK: Thickness of the shear wall member

VRBNAME: the standard rebar size of the vertical rebars in the shear wall member

VRBSPACE: the spacing of the vertical rebars in the shear wall member

ERBNAME: the standard size of the end rebars

ERBSPACE: the spacing size of the end rebars

iERBNUM: the number of end rebars

HRBNAME: the standard rebar size of the horizontal rebars in the shear wall member

HRBSPACE: the spacing of the horizontal rebars in the shear wall member

DE: Distance from the end of the shear wall member to the center of the first row of the vertical rebars {0}

DW: Distance from the center of the the end vertical rebars to the end of the shear wall {0}

* when using the initial value ??as the cover thickness, the value automatically calculated within the program will be used in the element design and strength inspection

*WALLMARK (Modify Wall Mark Data)

Group names or individual names for the purpose of classification of shear walls for automatic design or strength verification

; MARKNAME, WID_LIST

MARKNAME: Group or individual name that classifies the shear wall members

WID_LIST : List of shear wall member numbers

 

*SUP-EQ (Scale Up Factor for Earthquake)

The scale up factor in respect to the load combination that includes the

seismic load conditions and the seismic load. It is applied to the Chinese standards

; ELEM_LIST, LC-AXIAL, LC-MOMENT, LC-SHEAR, LCB

AXIAL, LCB-MOMENT, LCB-SHEAR

ELEM_LIST : element number

LC-AXIAL: the scale up factor in respect to the axial force of the

seismic load conditions

LC-MOMENT: the scale up factor in respect to the moment of the

seismic load conditions

LC-SHEAR: the scale up factor in respect to the shear force of the

seismic load conditions

LCB-AXIAL: the scale up factor in respect to the axial force of the load

combination that includes seismic loads

LCB-MOMENT: the scale up factor in respect to the moment of the load

combination that includes seismic loads

LCB-SHEAR: the scale up factor in respect to the shear force of the load

combination that includes seismic loads

*CUTLINE (Cutting Line)

Graphic output of internal forces of plate elements along a cutting line

; NAME, DIR, PT1X, PT1Y, PT1Z, PT2X, PT2Y, PT2Z, iR,iG, iB

NAME: name of Cutting Line to be registered

DIR: orientation of graphic output

= NORMAL: produce the graph normal to the plate elements

= INPLANE: produce the graph in the in-plane direction of the plate elements

PT1X: starting point of the Cutting Line

PT2X: end point of the Cutting Line

iR: color number of Red

iG: color number of Green

iB: color number of Blue

*CUTLINE2 (Plate Cutting Line Diagram)

Graphic output of internal forces of plate elements along a cutting line

; NAME, DIR, PT1X, PT1Y, PT1Z, PT2X, PT2Y, PT2Z, PT3X, PT3Y, PT3Z, iR, iG, iB

NAME: name of Cutting Line to be registered

DIR: orientation of graphic output

= NORMAL: produce the graph normal to the plate elements

= INPLANE: produce the graph in the in-plane direction of the plate elements

PT1X: starting point of the Cutting Line

PT2X: Coordinates defining the local x-direction vector

PT3X: Coordinates defining the local x-y plane vector

iR: color number of Red

iG: color number of Green

iB: color number of Blue

*UNKCONS (Unknown Load Factor Constraints)

Specifying the constraint conditions to be satisfied by the load

combination results, which include unknown load factors

; NAME, TYPE, iID, iPOINT, iCOMP, COND, bVALUE, VALUE, iOBJ

NAME: name of the constraint conditions

TYPE: type of the constraint conditions

 = REAC: Reaction

= DISP: Displacement

= TRUSS: Truss force

= BEAM: Beam force

iID: node (cooresponding element) number

iPOINT: selection of the location of the member force

iCOMP: selection of the member force component

COND: Equality/Inequality Condition

= LE: Less than or Equal to

= EQ: Equal to   = GE: Greater than or Equal to

bVALUE: option to enter Value (YES/NO)

VALUE: value to be satisfied for the reaction component

(displacement component, member force of truss or beam)

entered in the load combination, which includes unknown load factors

iOBJ: Other Node

*UNKFACTOR (Unknown Load Factor Data )

Creating new unknown load factor groups by entering the conditions to

obtain unknown load factors

; NAME=NAME, LCOMB, FTYPE, SIGN        ; 1st line

;      UNKCONS1, UNKCONS2, ..., UNKCONSn   

                                                                ; 2nd line

;      LCNAME1, WF1, LCNAME2, WF2, ...     ; from 3rd line

NAME: name of the unknown load factor group

LCOMB: load combination used to calculate the unknown load factors

¡Ø the load combination for calculating the unknown load factors must include

the load conditions determining the load factors

FTYPE: selecting the composition method of object fuctions composed of unknown

load factors

= LINEAR: load factor?the linear sum of the absolute values of the weight factors

 = SQUARE: load factor?the linear sum of the squares of the weight factors

= MAXIMUM: load factor?the max value of the absolute values of the weight factors

SIGN: assignment of the signs to the values calculated for the unknown load factors

= NEG: assigns the range of the value to minus (-)

= BOTH: assigns the range of the value to all ranges

= POS: assigns the range of the value to plus (+)

UNKCONS1: constraint conditions to be satisfied by the load combination results,

which include unknown load factorsLCNAME1: name of load case used as the

unknown load factor

WF1: scale factor, which is intended to adjust the relative importance of the

object function by assigning a weight factor to an unknown load factor

*BATCHCVT-MVLTRC (Batch Conversion from MVLRC to Static Load)

A number of loading conditions of different moving load locations are converted

into static loadings and produced as model files of the MCT type. This is an extremely ]useful feature when a number of loading conditions need to be converted. Conversion

is carried out by loading locations, result types, etc. all at once.

; NAME=NAME, TYPE                            ; 1st line;     

:NODE_OR_ELEMENT_LIST             ; 2nd line

;      bPART_I, bPART_1_4, bPART_1_2, bPART_3_4,

bPART_J                                                ; 3rd line

;      bFxx, bFyy, bFzz, bMxx, bMyy, bMzz, bVxx, bVyy

                                                             ; 4th line

;      MOVING_LC1, MINMAX1, ... , MOVING_LCn,

;      MOVING_LC1, MINMAX1, ... , MOVING_LCn,

MINMAXn                                             ; from 5th line

NAME: the name of the batch conversion

TYPE: Type of result

REAC: Reaction

DEFORM: Displacement

TRUSS_F: Truss Forces

Beam_F: Beam Forces

Plate_F: Plate Force

Beam_S: Beam Stresses

NODE_OR_ELEMENT_LIST: The list of the elements and nodes to be converted

bPART_I: the i-end of the beam element

bPART_1_4: the 1/4 position of the beam element

bPART_1_2: the 1/2 position of the beam element

bPART_3_4: the 3/4 position of the beam element

bPART_J: the j-end of the beam element

bFxx: Fxx of the plate element forces

bFyy: Fyy of the plate element forces

bFzz: Fzz of the plate element forces

bMxx: Mxx of the plate element forces

bMyy: Myy of the plate element forces

bMzz: Mzz of the plate element forces

bVxx: Vxx of the plate element forces

bVyy: Vyy of the plate element forces

MOVING_LC1: the dynamic load condition results to be printed

MINMAX1: Min/Max of the dynamic load conditions

*HYD-NODE (Heat of Hydration Node )

Specifying the directional component of the nodes and stresses for which

the time history analysis results of a heat of hydration analysis will be produced

; NAME, iNODE, iCOMP

NAME: name of the graph of the time history analysis

iNODE: node number

iCOMP: stress component

= 0 : Sig-XX

= 1 : Sig-YY

= 2 : Sig-ZZ

= 3 : Max (X, Y, Z)

*COLUMN-SHORTENING (Column Shortening )

Produce graphs for column shortening of a highrise structure resulting from a construction stage analysis

; NAME, X, Y, TOL, DISP-TYPE, CONST-STAGE

NAME: the name of the graph

X, Y: the location of the column in the global coordinates X & Y

TOL: the allowable tolerance

DISP-TYPE: type of displacement

CONST-STAGE: displacement resulting from a construction stage

*LOCALDIR-FSUM (Data for Local Direction Force Sum)

The load conditions and combination results of the local coordinate

; NAME=NAME, MODE, ANAL, LCB, TOL, bZVECTOR,

ZVX, ZVY, ZVZ                                ; 1st line

;      X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, ...      ; from line 2

NAME: load case

MODE: the method of selecting the subject plane that includes the nodes

where internal forces are to be combined}

ANAL: types of loads

LCB: load case

TOL: tolerence

BZVECTOR: Enter a vector to define the z-axis of the local coordinate system to

which Result Output is referenced  (YES/NO) {NO}

ZVX: the x-coordinates of the vertical vector of the surface

ZVY: the y-coordinates of the vertical vector of the surface

ZVZ: the z-coordinates of the vertical vector of the surface

X1: the coordinates of the first node in the x- direction in the global coordinate system

]Y1: the coordinates of the first node in the y- direction in the global coordinate system

Z1: the coordinates of the first node in the z- direction in the global coordinate system

Y2: the coordinates of the second node in the y- direction in the global coordinate system

Z2: the coordinates of the second node in the z- direction in the global coordinate system

X3: the coordinates of the third node in the x- direction in the global coordinate system

Y3: the coordinates of the third node in the y- direction in the global coordinate system

Z3: the coordinates of the thi