Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds /

Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds /

Bibliographic Details
Main Author: Nugent, Jack
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Other Authors: Pendergraft, Odis C.
Format: Government Document Book
Language:English
Published: [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1987.
Series:NASA technical paper ; 2588.
Subjects:
Aerodynamics, Transonic.
Reynolds number.

Evans: US Documents Microfiche (3rd floor)

Holdings details from Evans: US Documents Microfiche (3rd floor)
Call Number: NAS 1.60:2588
 
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NAS 1.60:2588 Available