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:
Physical Description:[108] σ. : εικ. ; 27 εκ.
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