Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique
Subtitle: progress report for the period ended June 30, 1994
By: by J.K. Ahuja, D.J. Singh, and S.N. Tiwari, principal investigator.
Contributors: Singh, David J. 1958-; Tiwari, S. N.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-197013.
Publisher: Old Dominion University Research Foundation; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: Norfolk, Va; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Axisymmetric flow.; Blunt bodies.; Bow waves.; Combustible flow.; Gas mixtures.; Hydrogen.; Hypersonic combustion.; Projectiles.; Shock layers.; Shock waves.; Viscous flow.
Other titles: Numerical simulation of shock induced combustion past blunt bodies using shock-fitting technique.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0269-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.