Summary
The boundary layer method for computing two-dimensional, compressible, laminar and turbulent boundary layers has been applied to a non-equilibrium boundary layer with an adverse pressure gradient.
Due to the fact that the boundary layer method provides results on a ”free-of-numerical-dissipation” basis, the influence of different turbulence models on the solution is investigated without being swamped by artificial viscosity.
In addition to solutions by other ETMA-workshop contributors — including Navier-Stokes solutions — the results provided in the present contribution are seen as an additional tool to properly describe the boundary-layer flow for the Stanford 80/81, Samuel-Joubert, CTF0141, test case.
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© 1998 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden
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Haase, W., Horton, H.P. (1998). The Samuel-Joubert Test Case Computed by a Boundary-Layer Method. 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_23
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DOI: https://doi.org/10.1007/978-3-322-89859-3_23
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-322-89861-6
Online ISBN: 978-3-322-89859-3
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