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:
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245 1 0 |a Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41/  |c John M. Smith and Albert J. Juhasz 
260 |a Washington:  |b National Aeronautics and Space Administration, Scientific and Technical Information Office,  |c 1978 
300 |a 37 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA technical paper  |v 1194 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Airplanes  |x Turbojet engines 
700 1 |a Junasz, Albert J.  |x Combustion 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Office 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Office 
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