A preliminary design study of supersonic through-flow fan inlets
By: Paul J. Barnhart.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- 182224.; NASA contractor report -- NASA CR-182224.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1988
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic drag.; Engine design.; Inlet flow.; Mach number.; Supersonic flow.; Turbofan engines.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 1 microfiche.