Numerical simulation of Mach reflection in steady flows

Author:

Schmisseur J. D.,Gaitonde D. V.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Reference36 articles.

1. Hadjadj A., Dussauge J.P.: Shock wave boundary layer interaction. Shock Waves 19(6), 449–452 (2009)

2. Schmisseur, J.D., Gaitonde, D.V.: Numerical investigation of new topologies in strong crossing shock-wave/ turbulent boundary-layer interactions. Paper 2000-0931, AIAA 38th Aerospace Sciences Meeting, Reno, NV, January 2000

3. Zheltovodov, A.A., Maksimov, A.I.: Hypersonic crossing-shock-waves/turbulent boundary layer interactions. Technical Report Final Report, EOARD Contract F61775-98-WE091, Russian Academy of Sciences, Novosibirsk, Russia (1999)

4. Schuelein, E., Zheltovodov, A.A.: Development of experimental methods for the hypersonic flows studies in Ludwieg tube. In: Proceedings of the International Conference on the Methods of Aerophysical Research: Part 1, pages 191–199. Institute of Theoretical and Applied Mechanics (1998)

5. Henderson L.F., Lozzi A.: Further experiments on transition of Mach reflection. J. Fluid Mech. 94, 541–559 (1979)

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