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The effect of surface temperature and reynolds number on the leeward heat-transfer for a shuttle orbiter
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Willman, R. B. Senalug, G. Bertin, J. J. McBride, M. |
| Copyright Year | 1975 |
| Description | The effect of windward surface temperature on the heat transfer to the leeward surface of the shuttle orbiter was investigated. Heat-transfer distributions, surface-pressure distributions, and schlieren photographs were obtained for an 0.01-scale model of the 37-0 shuttle orbiter at angles-of-attack of 30 deg and of 40 deg. Similar data were obtained for a fuselage-only configuration at angles-of-attack of 30 deg and of 90 deg. Data were obtained for various Mach numbers, Reynolds numbers, and surface temperatures. |
| File Size | 21832239 |
| Page Count | 154 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750014294 |
| Archival Resource Key | ark:/13960/t6741jk2k |
| Language | English |
| Publisher Date | 1975-04-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Reynolds Number Pressure Distribution Surface Temperature Angle of Attack Space Shuttle Orbiters Spacecraft Configurations Heat Transfer Mach Number 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 |
