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Wind-tunnel force and flow visualization data at mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from minus 4 deg to 60 deg
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Landrum, E. J. Babb, C. D. |
| Copyright Year | 1979 |
| Description | Flow visualization and force data for a series of six bodies of revolution are presented without analysis. The data were obtained in the Langley Unitary Plan wind tunnel for angles of attack from -4 deg to 60 deg. The Reynolds number used for these tests was 6,600,000 per meter. |
| File Size | 130069781 |
| Page Count | 268 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790013871 |
| Archival Resource Key | ark:/13960/t3421s45n |
| Language | English |
| Publisher Date | 1979-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Missile Configurations Tables Data Wind Tunnel Tests Flow Visualization Bodies of Revolution Angle of Attack Aerodynamic Forces Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
