3D 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 -- 107123.
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: Boundary layer separation.; Boundary layers.; Computational fluid dynamics.; Computational grids.; Engine inlets.; Flow distribution.; Internal flow.; Leading edges.; Navier-Stokes equation.; Shock wave interaction.; Shock waves.; Supersonic diffusers.; Three dimensional flow.; Turbulence models.
Other titles: 3D Navier Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0466-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1996] 1 microfiche.