Low-speed wind tunnel tests of a 50.8-centimeter (20-in.) 1.15-pressure-ratio fan engine model / by Howard L. Wesoky [and others]

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Corporate Authors:	Lewis Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Wesoky, Howard L.
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-3062.
Subjects:	Airplanes > Turbofan engines > Testing. Airplanes > Turbojet engines > Air intakes. Airplanes > Motors > Thrust. Short take-off and landing aircraft.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:3062
NAS 1.15:3062	Available Place a Hold