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Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5/

Main Author:	Mack, Robert J.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Division, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, Langley Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988
Series:	NASA technical paper 2799
Subjects:	Airplanes > Wings

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