Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing /

Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing /

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Bibliographic Details
Main Authors:	Powers, Sheryll Goecke (Author), Webb, Lannie D. (Author)
Corporate Authors:	United States National Aeronautics and Space Administration (sponsoring body.), NASA Dryden Flight Research Center
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1997
Series:	NASA technical memorandum ; 4789 NASA technical memorandum 4789
Subjects:	Boundary layers F-111 aircraft Pressure distribution Supercritical wings Wing camber
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Stanford University

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Call Number:	ISIL:US-CST