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Inclusion of transverse shear deformation in the exact buckling and vibration analysis of composite plate assemblies
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kennedy, David Anderson, Melvin S. |
| Copyright Year | 1993 |
| Description | The problem considered is the development of the necessary plate stiffnesses for use in the general purpose program VICONOPT for buckling and vibration of composite plate assemblies. The required stiffnesses include the effects of transverse shear deformation and are for sinusoidal response along the plate length as required in VICONOPT. The method is based on the exact solution of the plate differential equations for a composite laminate having fully populated A, B, and D stiffness matrices which leads to an ordinary differential equation of tenth order. |
| File Size | 1551276 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930017886 |
| Archival Resource Key | ark:/13960/t3nw4cs6r |
| Language | English |
| Publisher Date | 1993-05-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Dynamic Structural Analysis Stiffness Matrix Plate Theory Plates Structural Members Structural Vibration Differential Equations Laminates Buckling Computer Programs Shear Strain 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 |