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Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds/

Main Author:	Stallings, Robert L.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center
Other Authors:	Lamb, Milton, Watson, Carolyn B.
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1980
Series:	NASA technical paper 1683
Subjects:	Airplanes > Wings Stability of airplanes

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