The Langley 14- by 22-foot subsonic tunnel : description, flow characteristics, and guide for users /

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
Other Authors: Gentry, Garl L.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1990
Series:NASA technical paper 3008
Subjects:
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490 0 |a NASA technical paper  |v 3008 
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650 0 |a User requirements 
650 0 |a Wind tunnel apparatus 
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710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Division 
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