Flowfield measurements in the vortex wake of a missile at high angle of attack in turbulence
Approved for public release; distribution is unlimited === The flowfield downstream of a vertically-launched surface-to-air missile model at an angle of attack of 50° and a Reynolds number of 1.1 x 10(5) was investigated in a wind tunnel of the Naval Postgraduate School. The goal of this thesis is t...
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| Format: | Others |
| Language: | en_US |
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Monterey, California. Naval Postgraduate School
Dece
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| Online Access: | http://hdl.handle.net/10945/23235 |