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Effect of leading-edge load constraints on the design and performance of supersonic wings/

Main Author:	Darden, Christine M.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
Series:	NASA technical paper 2446
Subjects:	Airplanes > Wings Aerodynamics, Supersonic

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