A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 /

A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 /

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Bibliographic Details
Main Author: Ashby, George C.
Corporate Authors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1980.
Series:NASA technical paper ; 1787.
Subjects:
Sonic boom.
Aerodynamics, Supersonic.

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Call Number: NAS 1.60:1787
 
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NAS 1.60:1787 Available