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Title:
SUPERSONIC FLYING WING
Document Type and Number:
WIPO Patent Application WO/2010/129210
Kind Code:
A3
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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Inventors:
ZHA GECHENG (US)
Application Number:
PCT/US2010/032350
Publication Date:
March 10, 2011
Filing Date:
April 26, 2010
Export Citation:
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Assignee:
UNIV MIAMI (US)
ZHA GECHENG (US)
International Classes:
B64C30/00; B64C1/40; B64C3/10; B64D27/02
Foreign References:
US5730391A1998-03-24
US20050230531A12005-10-20
US4417708A1983-11-29
Attorney, Agent or Firm:
CHRISTOPHER, John et al. (P.A.200 East Las Olas Boulevard, Suite 204, Fort Lauderdale Florida, US)
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