
Pushover Global
Control dialog box
[Initial
Load]
Define, modify or
delete the initial load cases, which will be applied prior to
pushover analysis.
Perform Nonlinear
Static Analysis for Initial Load
This is the general way of applying the initial load.
Import Static Analysis
/ Construction Stage Analysis Results
1. When the boundary conditions are different between the initial
load and the pushover load.
2. To use the result from the final construction stage as the
initial load.
Note 1
When
using the result from the final construction stage as the initial
load for the pushover analysis, the member forces from the construction
stage analysis will be imported and nonlinear analysis will not
be performed for the initial load.
Note 2
For
the following cases, nonlinear analysis will not be performed
for the initial load but the result from the static analysis will
be imported for the pushover analysis.
-
When the boundary conditions/section stiffness scale factors are
different between the initial load and the pushover load
-
When using the member forces from the final construction stage
as the initial load for the pushover analysis Type your drop-down
text here.
Load Case
Select the load cases, which are
to be defined as the initial load for pushover analysis, among
the load cases applied to static analysis.
Scale Factor
Enter the magnification/reduction
factors to be applied to each selected load case for the initial
load.
Note
1
If the following
temperature loads are entered as an Initial Load, pushover analysis
cannot be performed.
1. Beam Section
Temperature
2. Temperature Gradient
3. System Temperature
4. Nodal Temperature
5. Element Temperature
Note
2
The
member forces caused by the initial load (in general, the gravity
load) are added to the resulting member forces due to pushover
analysis. However, the displacements caused by the initial load
are not considered in the pushover analysis.
Note
3
If P-M interaction
is considered in the hinge properties, it is recommended to apply
the initial load.
Note
4
In
order to check the results due to initial load in the pushover
analysis, a linear static analysis for the load cases which are
defined as initial load should be performed.
[Analysis Stop
: Shear Component Yield]
Specify
the condition of termination for the Pushover analysis.
Analysis
Stop : Shear Component Yield
Beam/Column: Select this option
to automatically terminate pushover analysis if a shear hinge
in a beam or a column member occurs.
Wall: Select this option to
automatically terminate pushover analysis if a shear hinge in
a wall occurs.
Note
If
the analysis is automatically terminated due to yielding of shear
hinge, analysis results can be examined up to the last pushover
step.
[Nonlinear Analysis
Option]
Specify the maximum number of sub-iterations
and a tolerance limit for convergence criterion.
Permit Convergency Failure
By increasing the number of steps
in an iterative nonlinear analysis, the rate of convergence can
be improved. However if the number of steps is large, the analysis
could be very time-consuming.
When this option is checked on and
if the analysis results do not converge, midas automatically subdivides
the step at which divergence occurs. Therefore analysis can be
converged without increasing the number of steps. When this option
is checked off and if the analysis results do not converge, the
analysis will be terminated.
Max. Number of Sub-steps
It is maximum number of Sub-steps,
which are segmented from each increment step
Maximum Iteration
Enter the maximum number of sub-iterations
in an increment step for repetitive analyses to satisfy an equilibrium
condition of the structure.
Note
1
Specified number
of sub-iterations is applied to all the pushover load cases.
Note
2 Unbalanced force and calculation
of the convergence
Convergence Criteria
Specify a tolerance limit for convergence.
If the incremental error falls within the tolerance, the iteration
stops within the corresponding analysis step prior to reaching
the maximum number of iterations and subsequent steps ensue.
Note
1
Convergence
Condition
There
are three convergence criteria (displacement norm, force norm
and energy norm) to check the convergence for an iterative process.
The user can select more than one norm to be reflected in the
iteration process.

Where, : Displacement
norm
:
Force norm
: Energy norm
: Effective load vector in the nth iteration step
: Incremental displacement vector in the nth iteration step
: Accumulated
Incremental displacement vector after n iterations
Note
2
In
general, applying displacement norm is enough. In a very special
case, an exact solution is not obtained because of remaining unbalanced
force is not negligible although they converge by the displacement
norm. In that case, the user may solve the problem by considering
additional criteria (force norm and energy norm)
Note
3
When multiple norms
are applied, the number of iterations in each increment step increases.
Note
4
When
the convergence tolerance is not satisfied, the remaining unbalanced
force is added to the external load in the subsequent step. Therefore,
if the analysis results are converged in the current step, the
failure of convergence in the previous step does not affect analysis
results.
[Pushover
Hinge Data Option]
Define the default stiffness reduction
ratio of the skeleton curve. Also specify the reference location
for calculating yield strength of beam element when the pushover
hinge property is defined as distributed type.
Default Stiffness
Reduction Ratio of Skeleton Curve
Specify the
stiffness reduction ratios after the 1st and 2nd yielding points
(1st yielding for bilinear curve, 1st and 2nd yielding for trilinear
curve) relative to the elastic stiffness when the skeleton curve
is Bilinear, Slip Bilinear, Trilinear type or Slip Trilinear type.
Trilinear / Slip Trilinear Type :
Specify the stiffness reduction
ratios after the 1st and 2nd yielding points for Trilinear curve.
α1:Stiffness
reduction ratio after the 1st yielding point (α1 ≤ 1.0)
α2:Stiffness
reduction ratio after the 2nd yielding point (α2
≤ α1 ≤ 1.0)
Bilinear / Slip
Bilinear Type : Specify the
stiffness reduction ratios after yielding point for Bilinear curve.
α1:Stiffness
reduction ratio after yielding point (α1 ≤ 1.0)

Note
If the user
changes the value of 'Default Stiffness Reduction Ratio of Skeleton
Curve' and click [OK] button, Stiffness Reduction Ratio is selected
as 'Use Value of Global Control Data' option in the Directional
Properties of Pushover Hinge dialog.
Point Spring
Support: Nonlinear Type
Nonlinear properties of Point Spring
Support (Comp.-only, Tens.-only, Multi-linear type) can be considered
in the pushover analysis.
Data for
Auto-Calculation of Capacity
Reference
Location only for Distributed Hinges
Specify the reference location (i-end,
j-end, center) for calculating yield strength of beam element
when the pushover hinge property is defined as distributed type.
Reference
Design Code (Eurocode 8: 2004)
Specify
scale factors for ultimate rotation and identify secondary seismic
elements. (Eurocode 8 only)
Scale
Factor for Ultimate Rotation : When calculating the total
chord rotation capacity at ultimate of concrete members, following
conditions can be considered as per A.3.1.1, ANNEX A, Eurocode
8-3.
Cold-worked
brittle steel
Without
detailing for earthquake resistance
Smooth
longitudinal bars

Secondary
Seismic Elements: Identify secondary seismic elements,
if any, by selecting predefined Structure Group.
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