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Structural analysis of ultra-high speed aircraft structural components
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lenzen, K. H. Siegel, W. H. |
| Copyright Year | 1977 |
| Description | The buckling characteristics of a hypersonic beaded skin panel were investigated under pure compression with boundary conditions similar to those found in a wing mounted condition. The primary phases of analysis reported include: (1) experimental testing of the panel to failure; (2) finite element structural analysis of the beaded panel with the computer program NASTRAN; and (3) summary of the semiclassical buckling equations for the beaded panel under purely compressive loads. A comparison of each of the analysis methods is also included. |
| File Size | 8455925 |
| Page Count | 144 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780005533 |
| Archival Resource Key | ark:/13960/t3906xd45 |
| Language | English |
| Publisher Date | 1977-12-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Dynamic Structural Analysis Finite Element Method Skin Structural Member Nastran Buckling Aircraft Structures Hypersonic Aircraft Wing Panels Destructive Tests 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 |
