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A local solution method for shock boundary-layer interaction on a swept wing

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Summary

The paper describes a local solution method for the calculation of the interaction between a weak shock front and a turbulent boundary layer on a swept wing. A multiple-deck approach allows the simplification of the governing equations according to the physical character of each deck. The mathematical model is based upon small-perturbation theory. The final boundary-layer solution is given by an iterative coupling of the solutions for each domain. The results are compared with experiments and with other theoretical solutions.

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  1. P. -Ch. Nellner &  J. Zierep

    Present address: Institut für Strömungslehre und Strömungsmaschinen, Universität Karlsruhe, D-76131, Karlsruhe, Kaiserstrasse 12, Germany

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    1. P. -Ch. Nellner
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    2. J. Zierep
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    Nellner, P.C., Zierep, J. A local solution method for shock boundary-layer interaction on a swept wing. Acta Mechanica 101, 45–57 (1993). https://doi.org/10.1007/BF01175596

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