SUPERSONIC FLYING WING
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United States of America Patent
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app pub date -
Apr 26, 2010
filing date -
Apr 27, 2009
priority date (Note) -
Abandoned
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Abstract
A bidirectional flying wing maximizes efficiency and reduces sonic boom during supersonic flight. The flying wing has bilateral symmetry across two perpendicular planes and a substantially isentropic compression bottom surface that minimizes the shock wave projected downward during flight. The flying wing may be rotated to provide a high aspect ratio and a low sweep angle during subsonic flight. The flying wing may be rotated to provide a low aspect ratio and a high sweep angle during supersonic flight.
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