Flowfield computations over the space shuttle Orbiter with a proposed canard at a Mach number of 5.8 and 50 degrees angle of attack

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Author
Reuter, William H., IV
Date
1993-06Advisor
Howard, Richard M.
Hobson, Garth V.
Buning, Pieter G.
Metadata
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Approved for public release; distribution is unlimited.