Mach 10 computational study of a three-dimensional scramjet inlet flow field
By: Scott D. Holland.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 4602.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamics.; Computational fluid dynamics.; Computational grids.; Hypersonic speed.; Inlet flow.; Navier-Stokes equation.; Shock wave interaction.; Supersonic combustion ramjet engines.; Supersonic inlets.; Three dimensional flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0478-M.

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