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Vladimir Gantovnik

Vladimir Gantovnik

Vladimir Gantovnik, Ph.D.
805 Lagoon Dr
Chula Vista CA 91910
(510)338-8seven11 
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Nastran allias in .cshrc PDF Print E-mail
Written by Administrator   
Monday, 16 January 2012 13:39

in .cshrc file:

alias na 'nastran 999.bdf que=nas_fast'

alias rmjunk 'rm *.log *.f04'

alias rmresults 'rm *.f04* *.f06* *.log* *.xdb *.op2 *.becho'

alias rmjpg 'rm *.jpg'

alias q 'que stat | pg'

alias qq 'que stat |grep g0068425'

 
Topology to CATIA PDF Print E-mail
Written by Administrator   
Friday, 13 January 2012 11:27
After topology optimization, new optimized topology of the part is obtained. The optimized geometry can be imported into CAD to guide designer in part redesign.

Exporting optimized geometry to STL file:

For HEX mesh --
1. Smooth the optimized design in Patran (Tools/Design Study/Post-Process/FEM Smooth).
2. Skin the smoothed solid elements (Utilities/FEM-Element/Skin Solid Elements).
3. Split the surface quad elements to tri elements (Elements/Modify/Quad/Split).
4. Export tri elements to STL file (Utilities/File/Export Import STL Files).

For TET mesh --
1. Skin the optimized solid mesh (Utilities/FEM-Element/Skin Solid Elements)
2. Export tri elements to STL file (Utilities/File/Export Import STL Files)

Importing STL file into CATIA:

1. Obtain STL Rapid Prototyping license (Tools/Options/General/Sharable Products/STL Rapid Prototyping).
2. Strat Machining_STL Rapid Prototyping.
3. Import STL file (Insert/STL Import).

For users who do not have CATIA STL Rapid Prototyping license, iges file can be used:

1. Skin the optimized solid mesh (Utilities/FEM-Element/Skin Solid Elements).
2. Create geometry from surface mesh (Utilities/Geometry/Create Surfaces from Shell Elemenrts).
3. Export iges file (File/Export/IGES). This file can be opened in CATIA.
 
What analysis capabilities are supported in optimization? PDF Print E-mail
Written by Administrator   
Friday, 13 January 2012 11:44

What analysis capabilities are supported in optimization?

MSC/NASTRAN optimization is multi-disciplinary. It supports both sizing and shape optimization. Below is a summary of the analysis type supported.

Sizing optimization:

statics
normal modes
buckling
modal frequency response
direct frequency response
modal transient response
static aero
flutter

Shape optimization:

statics
normal modes
buckling
modal frequency response
direct frequency response
modal transient response


Multiple boundary conditions:

statics
normal modes
buckling
flutter

 
How to have Patran set up a basic SOL 200 optimization run for Nastran? PDF Print E-mail
Written by Administrator   
Friday, 13 January 2012 11:24

How to have Patran set up a basic SOL 200 optimization run for Nastran?

Here is the rough procedure based upon Patran V2001:

1) Once the model is set up, go to TOOLS -- Model Variables

2) Set action/object/method to: Create Variable Property (or beam dimension or material depending on what your design variables to be). You can create as many design variables as you like linked to various shell, beam or material properties.

3)Once all the design variables are defined, go to TOOLS -- DESIGN STUDY

4) On this form, select the design variables you want to use in this optimization, the design objective and design constraints. In Patran, you are limited to design objectives of weight or volume. However, from the bulk data deck, you can create objectives for almost anything. Patran is giving you access to the basics of SOL 200, but not the complete set. Also, avoid setting the upper or lower bounds of constraints to 0.0 since that can cause numerical difficulties for the optimizer. If you really have a constraint where you need 0.0 to be the lower or upper bound, there are ways of dealing with this in the bulk data, but not through Patran.

5) Once you have applied the design study, go to the ANALYSIS form. Then select: Optimize Entire Model. Under translation parameters, select OP2 and Print instead of the default of XDB and print. If you use OP2 output for post processing, you will automatically get plots for the design variable history and objective function history created in Patran when you import the OP2 results file.

6) Once the job is run, you can browse the .f06 file for your results. The end of the .f06 file will contain the design variable history. A page or two above that will be the objective function history. After the design variable history printout, pay attention to the user information messages. There will be a message telling you why the job finished...e.g. Converged to a feasible design, or converged to the best compromise infeasible design.

 
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