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Aerodynamics of 3-dimensional bodies in transitional flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Potter, J. Leith |
| Copyright Year | 1987 |
| Description | Based on considerations of fluid dynamic simulation appropriate to hypersonic, viscous flow over blunt-nosed lifting bodies, a method was presented earlier for estimating drag coefficients in the transitional-flow regime. The extension of the same method to prediction of lift coefficients is presented. Correlation of available experimental data by a simulation parameter appropriate for this purpose is the basis for the procedure described. The ease of application of the method makes it useful for preliminary studies which involve a wide variety of three-dimensional vehicle configurations or a range of angles of attack of a given vehicle. |
| File Size | 609292 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870019996 |
| Archival Resource Key | ark:/13960/t54f6pb0x |
| Language | English |
| Publisher Date | 1987-10-11 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Three Dimensional Bodies Hypersonic Speed Aerodynamic Configurations Fluid Dynamics Drag Simulation Lifting Bodies Blunt Bodies Transition Flow Angle of Attack Viscous Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
