Research Catalog

Title

Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster.

Author

DeBonis, J. R.

Publication

[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Aeronautics and Space Administration, distributor], 1996.

Details

Additional Authors

• Yungster, S.
• Lewis Research Center. Institute for Computational Mechanics in Propulsion.

Description

1 v.

Series Statement

• NASA technical memorandum ; 107274
• ICOMP ; 96-6

Alternative Title

Rocket based combined cycle engine technology development

Subject

• Rocket engine design
• Rocket engines
• Engine inlets
• Navier-Stokes equation
• Computational fluid dynamics
• Flow distribution
• Pressure distribution
• Static pressure
• Computational grids
• Hypersonic flow

Note

• Shipping list no.: 98-0769-M.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.15:107274

OCLC

marcive41375980

Author

DeBonis, J. R.

Title

Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster.

Imprint

[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Aeronautics and Space Administration, distributor], 1996.

Series

NASA technical memorandum ; 107274

ICOMP ; 96-6

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.

Added Author

Yungster, S.

Lewis Research Center. Institute for Computational Mechanics in Propulsion.

Report No.

AIAA-96-3145

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:107274

Research Call Number

READEX Microfiche NAS 1.15:107274