Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
By: Scott D. Holland.
Contributors: Langley Research Center.
Series: NASA technical paper -- 3476.
Publisher: National Aeronautics and Space Administration, Langley Research Center; NASA Center for AeroSpace Information, distributor; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; Linthicum Heights, MD; Springfield, Va
Language: eng
Format: Microform
Subjects: Engine design.; Flow distribution.; Hypersonic inlets.; Hypersonic speed.; Inlet flow.; Internal flow.; Shock wave interaction.; Supersonic combustion ramjet engines.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0495-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.