Summary
A mathematically simple, turbulence closure model designed to treat transonic airfoil flows even with massive separation is described. Numerical solutions of the Reynolds-averaged, Navier-Stokes equations obtained with this closure model are shown to agree well with experiments over a broad range of test conditions.
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References
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© 1986 Springer-Verlag Berlin, Heidelberg
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Johnson, D.A., King, L.S. (1986). Transonic Separated Flow Prediction Based on a Mathematically Simple, Nonequilibrium Turbulence Closure Model. In: Délery, J. (eds) Turbulent Shear-Layer/Shock-Wave Interactions. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-82770-9_3
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DOI: https://doi.org/10.1007/978-3-642-82770-9_3
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-82772-3
Online ISBN: 978-3-642-82770-9
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