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Transonic performance of a mach 2.65 auxiliary flow axisymmetric inlet/

Main Author:	Santman, Don M.
Corporate Authors:	United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Ellco Engineering, Inc., Ames Research Center
Format:	Book
Language:	English
Published:	Washington, D.C.: National Aeronautics and Space Administration, 1976
Series:	NASA contractor report NASA CR-2747
Subjects:	Jet engines > Air intakes Aerodynamics, Transonic

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