Abstract
This work is interested in the design of discretization tools ensuring high order of accuracy for both discontinuous and smooth solutions. These developments are motivated by the desire to achieve aeroacoustic calculations of supersonic turbulent flows such as for instance supersonic jets, transonic airfoils or supersonic opened cavities.
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Berland, J., Le Garrec, T., Gloerfelt, X., Daru, V. (2009). Assessment of High-Order Algorithms for Aeroacoustic Computation of Shock-Containing Flows. In: Choi, H., Choi, H.G., Yoo, J.Y. (eds) Computational Fluid Dynamics 2008. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-01273-0_52
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DOI: https://doi.org/10.1007/978-3-642-01273-0_52
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