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Buclap2: a computer program for instability analysis of laminated long plates subjected to combined inplane loads
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tamekuni, M. Tripp, L. L. Halstead, D. W. Baker, L. L. |
| Copyright Year | 1973 |
| Description | This program description document describes the program structure and the design details of a CDC 6600 FORTRAN 4 digital computer program, BUCLAP2, which uses minimum energy principles to do an elastic stability analysis of curved and flat laminated rectangular long plates subjected to combined inplane normal and shear loads. Given the geometry, the material properties, and slected boundary conditions for the plate element, the program calculates the minimum buckling load for various wave lengths. The two parallel ends of the program calculates the minimum buckling load for various wave lengths. The two parallel ends of the long plate must be simply supported and arbitrary elastic boundary conditions may be imposed along either one or both external longitudinal sides. For guide to program use, see |
| File Size | 3078563 |
| Page Count | 99 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740005522 |
| Archival Resource Key | ark:/13960/t4qk26358 |
| Language | English |
| Publisher Date | 1973-08-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Plates Structural Members Laminates Buckling User Manuals Computer Programs Computer Programs Loads Forces Fortran Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
