Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /

Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /

Bibliographic Details
Main Author: Jenkins, Renaldo V.
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1983.
Series:NASA technical memorandum ; 85663.
Subjects:
Reynolds number.
Aerofoils > Testing.

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Call Number: NAS 1.15:85663
 
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NAS 1.15:85663 Available