Research Catalog

Title

A fully implicit time accurate method for hypersonic combustion [microform] : application to shock-induced combustion instability / Shaye Yungster and Krishnan Radhakrishnan.

Author

Yungster, Shaye.

Publication

Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

Details

Additional Authors

• Radhakrishnan, Krishnan.
• Lewis Research Center. Institute for Computational Mechanics in Propulsion.

Description

1 v.

Series Statement

NASA technical memorandum ; 106707

Subject

• Algorithms
• Combustion stability
• Computational fluid dynamics
• Hypersonic combustion
• Hypersonic speed
• Reacting flow
• Relaxation method (Mathematics)
• Shock wave interaction
• Transonic speed
• TVD schemes
• Unsteady flow
• Viscous flow

Note

• Distributed to depository libraries in microfiche.
• Shipping list no.: 95-0744-M.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.15:106707

OCLC

marcive33470037

Author

Yungster, Shaye.

Title

A fully implicit time accurate method for hypersonic combustion [microform] : application to shock-induced combustion instability / Shaye Yungster and Krishnan Radhakrishnan.

Imprint

Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

Series

NASA technical memorandum ; 106707

Reproduction

Microfiche. [Washington, D.C. : Supt. of Docs., U.S. G.P.O., 1995] 1 microfiche.

Added Author

Radhakrishnan, Krishnan.

Lewis Research Center. Institute for Computational Mechanics in Propulsion.

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:106707

Research Call Number

READEX Microfiche NAS 1.15:106707