Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

Bibliographic Details
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Other Authors: Lamb, Milton
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1979.
Series:NASA technical memorandum ; 80097.
Subjects:
Aerodynamics.

Evans: US Documents Microfiche (3rd floor)

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Call Number: NAS 1.15:80097/v.1-3
 
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