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.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Steffen, Fred W.
Corporate Authors:	Lewis Research Center, United States. National Aeronautics and Space Administration
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974.
Series:	NASA technical memorandum ; X-3064.
Subjects:	Airplanes > Turbofan engines. Airplanes > Nacelles. Airplanes > Motors > Thrust. Airplanes > Turbojet engines > Air intakes. Short take-off and landing aircraft.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:3064
NAS 1.15:3064	Available Place a Hold