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Transient analysis using conical shell elements
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Yang, J. C. S. Messick, W. T. Goeller, J. E. |
| Copyright Year | 1973 |
| Description | The use of the NASTRAN conical shell element in static, eigenvalue, and direct transient analyses is demonstrated. The results of a NASTRAN static solution of an externally pressurized ring-stiffened cylinder agree well with a theoretical discontinuity analysis. Good agreement is also obtained between the NASTRAN direct transient response of a uniform cylinder to a dynamic end load and one-dimensional solutions obtained using a method of characteristics stress wave code and a standing wave solution. Finally, a NASTRAN eigenvalue analysis is performed on a hydroballistic model idealized with conical shell elements. |
| File Size | 801585 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740006482 |
| Archival Resource Key | ark:/13960/t9479596b |
| Language | English |
| Publisher Date | 1973-09-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Numerical Analysis Conical Shells Structural Stability Eigenvalues Stress Waves Dynamic Loads Static Loads Computer Programs Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
