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Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41/

Main Author:	Smith, John M. 1922-
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lewis Research Center
Other Authors:	Junasz, Albert J.
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978
Series:	NASA technical paper 1194
Subjects:	Airplanes > Turbojet engines

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