Linear Static and Normal Nodes Analysis Using MSC/NASTRAN and MSC/PATRAN-NAS120

Table of Contents

Lesson Title

1. Submitting a MSC/NASTRAN Analysis: Review input file (.bdf) format, submit an input file to MSC/NASTRAN and review text result file (.f06) format.

2. Geometry Model of a 3-D Clevis: Learn how to make a new database, create a 3-D Clevis geometry and change graphics display.

 

3. Finite Element Model of a 3-D Clevis and Property Assignment: Define a finite element mesh for a 3-D Clevis and use mesh seeding for force loading in future exercises.

 

4. Loads and Boundary Conditions on a 3-D Clevis: Apply loading conditions and constraints to a 3-D Clevis.

 

5. Spatial Variation of Physical Properties: Learn how to create a circular plate with varying material and physical properties.

 

6. Using Groups and Lists: Learn to import or construct a fairing with curves and surfaces. Also apply 1-D elements that will represent structural stiffeners.

 

7. Post Processing of Stress Results: Examine the stress results of a Clevis model from MSC/NASTRAN code by rendering a variety of fringe and element fill plots.

 

8. Linear Static Analysis of a Simply-Supported Truss: Create a finite element truss with segments in tension or compression connected by smooth pins.

 

9. Linear Static Analysis of a Cantilever Beam (SI Units): Create and apply a pure bending load to a hollow, rectangular beam.

 

10. Linear Static Analysis of a Simply-Supported Stiffened Plate: Create a stiffened plate, prepare a MSC/NASTRAN input file for a Linear Static analysis and visualize results.

 

11. Linear Static Analysis of a Solid Lug: Create a geometrical cantilever lug, define nonuniform loads using Fields, prepare file for MSC/NASTRAN input and visualize analysis results.

 

12. Verification of a Stiffened Plate Model: Become familiar with MSC/NASTRAN error and warning messages arising from modeling mistakes.

 

13. Normal Modes Analysis of a Simply-Supported Stiffened Plate: Convert a Linear Static analysis input file to a Normal Modes analysis input file, generate weight information and review results.

 

14. Buckling Analysis of a Thin-Shell Cylinder: Create a thin-shell cylinder and prepare it for MSC/NASTRAN input file for Buckling analysis.

 

15. Restarting a Linear Static Analysis of a Simply-Supported Stiffened Plate: Restart previous Stiffened Plate for new load conditions.

 

16. Normal Modes - Rigid Element Analysis with RBE2 and CONM2: Create a geometric representation of a tube, define the model by plate elements, define the weights of the model and run normal modes analysis.

 

17. Linear Static - Rigid Element Analysis with RBE2 and CONM2: Run previous lessons using linear static analysis.

 

18. Modal Analysis of Interpolation Constraint Elements and Concentrated Mass: Replace rigid elements with interpolation constraint elements in lesson 16 and run again for modal analysis.

 

Appendix

A. Importing Geometry from an IGES file: Import geometry from IGES files, create a solid from CAD curves and surfaces and Tet mesh the solid.

 

B. Linear Static Analysis of a Cantilever Beam Using Beam Library (SI Units): Create and apply a pure bending load to a hollow, rectangular beam using beam library.

 

C. Normal Modes Analysis of a Simply-Supported Stiffened Plate: Convert a Linear Static analysis input file to a Normal Modes analysis input file, generate weight information and review results.

 

D. CBAR Element Shear Factor, K: Model a loaded cantilever beam with and without shear factors.

 

E. CBEAM Tapered Flanged Beam with Shear Relief: Create a loaded, tapered, flanged cantilever beam with and without shear relief.

 

F. Simple Lumped Mass System: Model a simple lumped mass system using beam elements and point elements, apply proper constraints to ensure stability during analysis and find the first two modes of vibration.

 


Support Files

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To MSC/NASTRAN Exercise Books

To MSC/PATRAN Main Directory

To MSC/PATRAN Exercise Books