Abstract
The supersonic flow over an axisymmetric rearward facing step, placed on the circumference of an axisymmetric body of a 6 in. diameter, has been experimentally investigated by Roshko and Thomke, [1]. Among other flow conditions, they have published measurements for three different step heights, namely 0.25, 1.02 and 1.675 in., at an external flow Mach number equal to 2.09.
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References
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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). Supersonic Rearward-Facing Step Calculations using an Explicit Fractional-Step Method and a Two-Equation Turbulence Model. 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_10
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DOI: https://doi.org/10.1007/978-3-322-89859-3_10
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
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