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The structural finite element model of the c-5a
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McClellan, G. W. |
| Copyright Year | 1985 |
| Description | A substructured NASTRAN model of the C-5A was analyzed for several different load conditions. The size of the model and the number of load cases used presented special problems in computer file and space management. This resulted in revisions to the in-house NASTRAN code. Despite the problems encountered the analyses were completed with excellent results. |
| File Size | 450651 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850017574 |
| Archival Resource Key | ark:/13960/t8nd0v01v |
| Language | English |
| Publisher Date | 1985-05-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Finite Element Method Airframes Computer Techniques Lockheed Aircraft Dynamic Loads Nastran Cargo Aircraft C-5 Aircraft Computer Aided Design Structural Analysis Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |