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A finite element program for postbuckling calculations (pstbkl)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carlson, R. L. Simitses, G. T. Riff, R. |
| Copyright Year | 1991 |
| Description | The object of the research reported herein was to develop a general mathematical model and solution methodologies for analyzing the structural response of thin, metallic shell structures under large transient, cyclic, or static thermochemical loads. This report describes the computer program resulting from the research. Among the system responses associated with these loads and conditions are thermal buckling, creep buckling, and ratcheting. Thus geometric and material nonlinearities (of high order) have been anticipated and are considered in developing the mathematical model. The methodology is demonstrated through different problems of extension, shear, and of planar curved beams. Moreover, importance of the inclusion of large strains is clearly demonstrated, through the chosen applications. |
| File Size | 34087790 |
| Page Count | 106 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920011342 |
| Archival Resource Key | ark:/13960/t7vm95f2z |
| Language | English |
| Publisher Date | 1991-12-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Curved Beams Applications of Mathematics Nonlinear Equations Structural Stability Elastic Buckling Creep Buckling Cyclic Loads Static Loads Finite Element Method Elastoplasticity Thin Walled Shells Temperature Effects Strain Distribution Mathematical Models Applications Programs Computers Transient Loads Thermal Buckling Buckling Constitutive Equations Loads Forces Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |