A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 [microform] / Richard J. Re and William K. Abeyounis.

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Bibliographic Details
Main Author: Re, Richard J.
Corporate Author: Langley Research Center
Other Authors: Abeyounis, William Kelly
Format: Government Document Microfilm Book
Language:English
Published: Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1996]
Series:NASA technical memorandum ; 110300.
Subjects:
Wind tunnel models.
Airplanes > Motors.
Mach number.
Aircraft engines.
Angle of attack.
Engine inlets.
Pressure distribution.
Subsonic flow.
Static pressure.
Wind tunnel tests.

Norlin Library - Government Information - Microform

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Call Number: NAS 1.15:110300
NAS 1.15:110300 Restricted Place a Hold

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