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

1993-06

Advisor

Howard, Richard M.

Hobson, Garth V.

Buning, Pieter G.

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Description

Approved for public release; distribution is unlimited.

URI

http://hdl.handle.net/10945/39837

Collections

• 1. Thesis and Dissertation Collection, all items