Summary
In this report we analyze the two-dimensional flow field generated by the reflection of an incident oblique shock wave on a flat wall, and its interaction with the turbulent boundary layer developing on the plate. The general features of the flow field are described, and the experimental measurements of Delery [1] are presented. Appropriate boundary conditions for the numerical calculation of this case are given.
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References
Delery J., Etude experimentale de la reflection d’une onde de choc sur une paroi chauffe en presence d’une couche limite turbulente, La Recherche Aerospatiale, 1, 1992.
Kline et. al.(ed.s), Proceedings of the 1980 HTTM Stanford Conference on Complex Turbulent Flows, Stanford University, 1981.
Fernholz H.H., Finley P.J., A further compilation of compressible boundary-layer data with a survey of turbulence data, AGARDograph 263, 1981.
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© 1998 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden
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Arina, R. (1998). ETMA Test Case 6 Shock Reflection on a Flat Plate Description of the Test Case. In: Dervieux, A., Braza, M., Dussauge, JP. (eds) Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA. Notes on Numerical Fluid Mechanics (NNFM), vol 5. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-322-89859-3_28
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DOI: https://doi.org/10.1007/978-3-322-89859-3_28
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-322-89861-6
Online ISBN: 978-3-322-89859-3
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