A fully implicit time accurate method for hypersonic combustion
Subtitle: application to shock-induced combustion instability
By: Shaye Yungster and Krishnan Radhakrishnan.
Contributors: Radhakrishnan, Krishnan.; Lewis Research Center. Institute for Computational Mechanics in Propulsion.
Series: NASA technical memorandum -- 106707.
Publisher: National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion; National Technical Information Service, distributor
Published: 1994
Place of publication: Cleveland, Ohio; [Springfield, Va
Language: eng
Format: Microform
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0744-M.

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