Analysis of pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered delta wing-body combination
An investigation was conducted in the Langley 8-foot transonic tunnels to determine the aerodynamic loading characteristics of a thin conical cambered low-aspect-ratio delta wing in combination with a basic body and a body indented symmetrically for a Mach number of 1.2 in accordance with the supers...
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| Format: | Others |
| Language: | en_US |
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Virginia Polytechnic Institute
2017
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| Online Access: | http://hdl.handle.net/10919/76118 |