A preliminary design study of supersonic through-flow fan inlets [microform] / Paul J. Barnhart.

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Bibliographic Details
Main Author:	Barnhart, Paul J.
Corporate Author:	United States. National Aeronautics and Space Administration
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], [1988]
Series:	NASA contractor report ; NASA CR-182224.
Subjects:	Aerodynamic drag. Engine design. Inlet flow. Mach number. Supersonic flow. Turbofan engines.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:182224
NAS 1.26:182224	Restricted Place a Hold