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

Bibliographic Details
Main Authors: Re, Richard J. (Author), Abeyounis, William Kelly (Author)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
Series:NASA technical memorandum ; 110300.
Subjects:
Aircraft engines.
Angle of attack.
Engine inlets.
Mach number.
Pressure distribution.
Subsonic flow.
Static pressure.
Wind tunnel tests.
Online Access:https://purl.fdlp.gov/GPO/LPS68006
Description
Item Description:"November 1996."
"Performing organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (180 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 12-13).