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Investigation of flow characteristics over missile bodies at supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sawyer, W. C. Barger, R. L. |
| Copyright Year | 1979 |
| Description | Three missile body shapes tested at Mach numbers of 1.50, 2.16, and 2.86 with angles of attack up to 30 degrees are described. The flow characteristics for each body shape are examined. The measured aerodynamic forces and moments are presented. The use of flow visualization techniques are described and the results such as vortex effects are discussed. |
| File Size | 10878043 |
| Page Count | 42 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800004746 |
| Archival Resource Key | ark:/13960/t19k94w6b |
| Language | English |
| Publisher Date | 1979-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Boundary Layer Separation Missile Configurations Supersonic Speed Missile Bodies Vortices Flow Distribution Vorticity Flow Visualization Separated Flow Cross 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 |
