Summary
Numerical results obtained for the hypersonic flow (M∞ = 8.25 and M∞ = 25) over a double ellipse are presented. Results are obtained using a Taylor-Galerkin finite element formulation. Non-structured grids of simple linear triangular 3 node elements are used. An Adaptive grid refinement technique based on a simple error estimator to improve the numerical solution near shocks is used.
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© 1991 Springer-Verlag Berlin Heidelberg
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Oñate, E., Quintana, F., Miquel, J. (1991). Numerical Simulation of Hypersonic Flow over a Double Ellipse using a Taylor-Galerkin Finite Element Formulation with Adaptive Grids. 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_43
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DOI: https://doi.org/10.1007/978-3-642-76527-8_43
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