Cruise performance of an isolated 1.15 pressure ratio turbofan propulsion system simulator at Mach numbers from 0.6 to 0.85, by Fred W. Steffen et al.

Title:	Cruise performance of an isolated 1.15 pressure ratio turbofan propulsion system simulator at Mach numbers from 0.6 to 0.85
Author:	Steffen, Fred W.
Author:	Lewis Research Center
Note:	National Aeronautics and Space Administration ;, 1974

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Subject:	Airplanes -- Motors -- Thrust
Subject:	Airplanes -- Nacelles
Subject:	Airplanes -- Turbofan engines
Subject:	Airplanes -- Turbojet engines -- Air intakes
Subject:	Short take-off and landing aircraft
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