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A wind-tunnel investigation of the aerodynamic characteristics of bodies of revolution at mach numbers of 2.37, 2.98, and 3.90 at angles of attack to 90 deg
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1960 |
| Description | High angle aerodynamic characteristics produced by nose cone of revolution in wind tunnel at supersonic speed |
| File Size | 1327566 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650014315 |
| Archival Resource Key | ark:/13960/t41s1j30g |
| Language | English |
| Publisher Date | 1960-08-01 |
| Access Restriction | Open |
| Subject Keyword | Nose Cone Supersonic Wind Tunnel Supersonic Speed Aerodynamic Characteristics Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |