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:
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