An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 /

Bibliographic Details
Main Author:	Re, Richard J.
Corporate Author:	Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Washington : U.S. National Aeronautics and Space Administration ; 1976.
Series:	NASA technical memorandum ; NASA TM X-3324.
Subjects:	Mach number. Aerofoils. Airplanes > Turbojet engines > Air intakes.

Evans: US Documents (Annex 5th floor)