Abstract
The use of unstructured polygonal meshes for the solution of the 2D compressible Euler equations is described together with a solution adaptive grid refinement strategy which enables better shock capturing. Results are shown for the double ellipse test cases 6.1.1 and 6.1.3.
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© 1991 Springer-Verlag Berlin Heidelberg
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Vankeirsbilck, P., Deconinck, H. (1991). Computation of 2D Inviscid Hypersonic Flows Using Unstructured Polygonal Meshes. In: Désidéri, JA., Glowinski, R., Périaux, J. (eds) Hypersonic Flows for Reentry Problems. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-76527-8_29
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DOI: https://doi.org/10.1007/978-3-642-76527-8_29
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