Performance and surge limits of a TF30-P-3 turbofan engine/axisymmetric mixed-compression inlet propulsion system at Mach 2.5 /
Joseph F. Wasserbauer, Harvey E. Neumann, and Robert J. Shaw.

Description

Main Author: Wasserbauer, Joseph F.
Related Names: Shaw, Robert J. (Robert Joseph), 1946-
Neumann, Harvey E.
Lewis Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1985.
Subjects: Aerodynamics, Supersonic.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Air intakes.
Airplanes > Airplanes / Turbofan engines > Airplanes / Turbofan engines / Testing.
Note: Prepared at Lewis Research Center.
"May 1985"--Cover.
Physical Description: 18 p. : ill. ; 28 cm.
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