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Body and canard effects on an attached-flow maneuver wing at Mach 1.62/

Main Author:	Pittman, James L.
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
Other Authors:	Miller, David S., Mason, William H.
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984
Series:	NASA technical paper 2249
Subjects:	Airplanes > Wings, Canard Aerodynamics, Supersonic

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