Research Catalog

Title

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet [microform] / M. Mizukami and J.D. Saunders.

Author

Mizukami, M.

Publication

[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors

• Saunders, J. D.
• United States. National Aeronautics and Space Administration.

Description

1 v.

Series Statement

NASA technical memorandum ; 107123

Alternative Title

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

Subject

• 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

Note

• Distributed to depository libraries in microfiche.
• Shipping list no.: 96-0466-M.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.15:107123

OCLC

marcive35282961

Author

Mizukami, M.

Title

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet [microform] / M. Mizukami and J.D. Saunders.

Imprint

[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Series

NASA technical memorandum ; 107123

Reproduction

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

Added Author

Saunders, J. D.

United States. National Aeronautics and Space Administration.

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:107123

Research Call Number

READEX Microfiche NAS 1.15:107123