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Nastran static and buckling analysis - comparison with other large-capacity programs
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Shah, L. C. |
| Copyright Year | 1973 |
| Description | A square plate with clamped edges under a concentrated load was modeled using NASTRAN and ASKA finite element computer programs. Deflections were computed for various width-to-thickness ratios (b/t) of the plate element, and were compared against the classical theory to determine the b/t limitations. A cylinder with simply supported ends was modeled using NASTRAN and STAGS computer programs for buckling analysis. The models were subjected to a uniform radial pressure loading. Several parameters were changed, and the effects of those variations are presented. Utilizing these data, a model which will produce results comparable to published empirical data can be constructed and processed for a minimized cost. |
| File Size | 674730 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740006478 |
| Archival Resource Key | ark:/13960/t5m950b07 |
| Language | English |
| Publisher Date | 1973-09-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Rectangular Plates Finite Element Method Bending Moments Stress Analysis Numerical Analysis Structural Stability Materials Tests Elastic Properties Buckling Computer Programs Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |