Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 /

Bibliographic Details
Main Author:	Capone, Francis J.
Corporate Author:	Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Washington : U.S. National Aeronautics and Space Administration ; 1976.
Series:	NASA technical memorandum ; NASA TM X-3313.
Subjects:	Airplanes > Jet propulsion. Nozzles > Testing.

Evans: US Documents (Annex 5th floor)