Abstract
The problems, which interest CEA/DAM for atmospheric reentry of strategic missile, need robust hypersonic codes because they have to consider complex physical models around various configurations. The high magnitude reached by the temperatures, oblige us to take into account the dissociation of air molecules, the ionization and the wall ablation effects.
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References
B. Stoufflet, J. Periaux, F. Fezoui, A. Dervieux Numerical Simulation of 3D Hypersonic Euler Flows Around Space Vehicles Using Adapted Finite Elements - AIAA 25th Aerospace Sciences Meeting - January 12–15, 1987, Reno Nevada
H.C. Yee - Upwind and Symmetric Shock-Capturing Schemes - NASA Technical Memorandum 89464
R.W. Mac Cormack, G. Candler - Hypersonic Flows past 3D Con-figurations - AIAA paper 87 - 0480.
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© 1991 Springer-Verlag Berlin Heidelberg
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Angrand, F., Tessieras, B., Dubroca, B., Morreeuw, J.P. (1991). Hypersonic Flows Over a Double or Simple Ellipse. 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_39
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DOI: https://doi.org/10.1007/978-3-642-76527-8_39
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-76529-2
Online ISBN: 978-3-642-76527-8
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