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