An edition of 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet (1995)

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

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3D Navier-Stokes analysis of a Mach 2.68 bifu ...
M. Mizukami
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January 22, 2010 | History
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An edition of 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet (1995)

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

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Publish Date
Publisher
National Aeronautics and Space Administration, National Technical Information Service, distributor
Language
English

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Subjects

Computational fluid dynamics Boundary layers Supersonic diffusers Computational grids Boundary layer separation Turbulence models Three dimensional flow Flow distribution Engine inlets Internal flow Leading edges Shock wave interaction Navier-Stokes equation Shock waves
Edition Availability
Cover of: 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
1995, National Aeronautics and Space Administration, National Technical Information Service, distributor
Microform in English
Cover of: 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
1995, National Aeronautics and Space Administration, National Technical Information Service, distributor
Microform in English

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Book Details

Edition 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.

Published in
[Washington, DC], [Springfield, Va
Series
NASA technical memorandum -- 107123
Other Titles
3D Navier Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

The Physical Object

Format
Microform
Pagination
1 v.

Edition Identifiers

Open Library
OL17117540M

Work Identifiers

Work ID
OL12015384W

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