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Results of heat transfer tests on a 0.0175-scale space shuttle orbiter model (56-0) in the aedc vkf 'b' hypersonic wind tunnel (oh74)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Dye, W. H. |
| Copyright Year | 1976 |
| Description | The results are presented of aerodynamic heating tests conducted on a 0.0175-scale model of the space shuttle orbiter. The tests were conducted at a nominal Mach number of 8 and model angles of attack varying between 20 deg and 45 deg. |
| File Size | 30949202 |
| Page Count | 588 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760014178 |
| Archival Resource Key | ark:/13960/t5z659m9z |
| Language | English |
| Publisher Date | 1976-02-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Tables Data Hypersonic Speed Scale Models Aerodynamic Heat Transfer Aerodynamic Heating Wind Tunnel Tests Hypersonic Heat Transfer Hypersonic Wind Tunnels Space Shuttle Orbiters Graphs Charts Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
