Mechanical APDL Structural Analysis Guide

(lily) #1
tolerance defaults to 0.0, so that the response first order eigenvalues can be used to more precisely
determine a new time step value.

Note

If you are using the Solution Controls dialog box to set solution controls, you can access
all of these options (ALPHAD,BETAD,KBC,TIMINT,TINTP,TRNOPT) on the Transient
tab.


  1. Write load data for each load step to a load step file.
    Command(s):LSWRITE
    GUI: Main Menu> Solution> Load Step Opts> Write LS File

  2. Save a backup copy of the database to a named file.
    Command(s):SAVE
    GUI: Utility Menu> File> Save As

  3. Start solution calculations. Other methods for multiple load steps are described in Getting Started in the
    Basic Analysis Guide.
    Command(s):LSSOLVE
    GUI: Main Menu> Solution> Solve> From LS Files

  4. After you have solved all load steps, leave SOLUTION.
    Command(s):FINISH
    GUI:Close the Solution menu.


8.7.3. Review the Results


As in a nonlinear static analysis, you can use POST1 to postprocess results at a specific moment in time.
Procedures are much the same as described previously for nonlinear static analyses. Again, you should
verify that your solution has converged before you attempt to postprocess the results.


Time-history postprocessing using POST26 is essentially the same for nonlinear as for linear transient
analyses. See the postprocessing procedures outlined in Transient Dynamic Analysis (p. 107).


More details of postprocessing procedures can be found in the Basic Analysis Guide.


8.8. Example Input for a Nonlinear Transient Analysis


Following is an example input listing for a nonlinear transient analysis:


! Build the Model:
/PREP7
---! Similar to a linear full transient model, with
---! these possible additions: nonlinear material
---! properties, nonlinear elements
---
FINISH
!
! Apply Loads and Obtain the Solution:
/SOLU
ANTYPE,TRANS
! TRNOPT,FULL by default
---! Establish initial conditions as in linear full
---! transient analysis
LSWRITE! Initial-condition load step

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Nonlinear Structural Analysis

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