Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By: M. Mizukami and J.D. Saunders.
Contributors: Saunders, J. D.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 107003
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Computational grids.; Inviscid flow.; Navier-Stokes equation.; Supersonic diffusers.; Supersonic inlets.; Turbulence models.; Two dimensional flow.
Other titles: Parametrics on 2D Navier Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0021-M.

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