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Finite element approach to the integrated potential formulation of general unsteady supersonic aerodynamics
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Appa, K. Smith, G. C. C. |
| Copyright Year | 1973 |
| Description | Analytical formulation of the integrated potential approach for general unsteady supersonic configurations is related to numerical solution approaches using an arbitrary finite element mesh. Work remains to be done on adequate numerical handling of singular integrals, discussed in an appendix. Limited results on a planar rectangular wing are presented. |
| File Size | 1244165 |
| Page Count | 38 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730013177 |
| Archival Resource Key | ark:/13960/t72v79n6r |
| Language | English |
| Publisher Date | 1973-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Finite Element Method Uncambered Wings Numerical Analysis Aerodynamic Configurations Body-wing Configurations Supersonic Flight Unsteady Aerodynamics Rectangular Wings Mathematical Models Aerodynamic Characteristics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
