Abstract
In this work, the low-Reynolds k-ε model, with or without Algebraic Reynolds Stress modifications will be used for the numerical modelling of the two-dimensional shock wave / turbulent boundary layer interaction problem, over compression ramps. Two different compression ramps will be used, with corner angles equal to 20 and 24 degrees, according to the experiments performed in the Princeton University [1], [2].
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© 1998 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden
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Vassilopoulos, C., Giannakoglou, K.C., Papailiou, K.D. (1998). Study of the Supersonic Compression Ramp Flow Using the k-ε Turbulence Model with and Without Algebraic Reynolds Stress Modifications. 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_34
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DOI: https://doi.org/10.1007/978-3-322-89859-3_34
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
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