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Load Case Name
Enter
the name of the response spectrum analysis case. The name
is used for load combinations. (Refer
to "Combinations")
Direction
X-Y: Apply the response
spectrum loads in the horizontal directions (directions
parallel to GCS X-Y plane) of the structure.
Z: Apply the response
spectrum loads in the vertical direction (GCS Z-direction)
of the structure.
Auto-Search
Angle
Select this option
to automatically take the excitation angle of response
spectrum as the major-axis direction of a building.
Major
: Major-axis direction
Ortho
: Major-axis direction + 90˚
Note
"Major"
and "Ortho" must be defined in the identical
Response Spectrum function. For example, if we define"RX"
load case as "Major", "RY" load case
must be defined as "Ortho". After performing
the Response Spectrum Analysis, excitation angle of the
structure will be automatically entered in the "Excitation
Angle" field.
Excitation
Angle
When
the seismic excitation direction is parallel to the X-Y
plane (Direction='X-Y'), the sign of the seismic loading
angle [Degree] is referenced to the Z-axis using the right
hand rule.
The
angle is zero at the GCS X-axis.
Scale
Factor
Scale
factor for the entered response spectrum excitation
Period
Modification Factor
A
multiplier factor for periods calculated by eigenvalue
analysis.
Non-structural
members are typically excluded in the analytical model,
but rather treated as loads. Such omission can result
in higher periods than actually are. This factor applies
to all the natural periods calculated by eigenvalue analysis
for response spectrum analysis. This functionality becomes
useful when we wish to account for stiffness contribution
of non-structural elements in which case we may wish to
reduce the calculated periods.
Note
This factor applies to all the natural periods calculated
by eigenvalue analysis for response spectrum analysis.
This functionality becomes useful for example when we
wish to account for stiffness contribution of non-structural
elements in which case we may wish to reduce the calculated
periods.
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Modal Combination Control
Enter the method of mode combination
and specify whether to restore the signs of response spectrum
analysis results. midas Gen allows the user to select the modes
for a modal combination so that the major modes of a structure
can be combined. [Details...]
Spectrum
Functions
Select pre-defined design spectrum
functions, which will be used to define a number of response spectrum
load cases. A same spectrum from a code may result in a number
of spectrum functions depending on the damping ratio. Therefore,
this becomes useful when the user wishes to define a number of
spectrum functions based on different damping values in a structure.
Function Name
Select
a spectrum function name. If spectral functions have not been
defined, click the
button located at the bottom of the dialog box to define spectrums.
(Refer to "Response
Spectrum Functions")
Generating spectrum data corresponding to damping ratios by modes
using multiple Response Spectrum Functions
Generating spectrum
data corresponding to damping ratios by modes using a single Response
Spectrum Function
Apply Damping Method
Damping
Method : Define the damping property of a structure using
multiple design spectrums.
Direct Modal
Mass and Stiffness Proportional
Strain Energy Prop
Correction
by Damping Ratio : When a single spectrum is selected,
a modifying equation is used to adjust the spectrum to apply to
each mode having

Note
1
The modifying equation can not be used when multiple spectrums
are selected because the spectrums are interpolated based on the
damping ratios. A damping ratio
can not go beyond the upper and lower bound damping ratios of
the spectrum.
Note
2
When combining modal responses, using Complete Quadratic Combination
(CQC) will reflect damping for each mode without the use of
the modifying equation. The combining
method can be specified in Modal Combination Control.
Interpolation of Spectral Data
Select the method of interpolating the response spectrum load
data.
Linear
: Linear interpolation method
Logarithm
: Log-scale interpolation method
Accidental Eccentricity
Select whether to include accidental eccentricity moments in
the calculation of response spectrum loads. Click
to prompt the Accidental Eccentricity for Response Spectrum Load
dialog box.
Note
1
Using this functionality, we can check the analysis results from
the auto-generated load case (Es: Dynamic load case name), which
reflects the accidental eccentric moments.
Note
2
The magnitudes of the applied accidental torsional moments can
be checked in Results > Result Tables > Story
Shear (Response Spectrum Analysis)
Note
3
This function becomes activated only when Model > Building >
Story Data
is defined.

Accidental
Eccentricity for Response Spectrum Load dialog box
Eccentricity Data
Automatic
An eccentricity in terms of a percentage
of plan dimensions is automatically considered.
User Defined
The user defines the eccentricities
individually.
Consider
Eccentricity below G.L
Check
on: Eccentricity is considered for both above-ground
and underground floors.
Check
off: Eccentricity is considered only for above-ground floors.
Description
Enter a brief description.
Operations
Enter
new or additional response spectrum analysis load cases
Enter the above entries and click
.
Modify
previously entered response spectrum analysis load cases
Select a response spectrum analysis
load case from the list in the dialog box and click .
Delete
previously entered response spectrum analysis load cases
Select a response spectrum analysis
load case from the list in the dialog box and click .
In addition to the spectrum functions
and the loading conditions of the response spectrum, access the
following functions to enter additional data required for a response
spectrum analysis:
:
Eigenvalue
Analysis Control... is invoked to check dynamic properties
of a structure
: Response Spectrum Functions...
is invoked to define spectrums.
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