Abstract
In this contribution to the Workshop on Hypersonic Flows for Reentry Problems, we are interested in showing that an implicit method without upwinding or flux limiter can calculate external flows at large Mach number, large angle of attack and large Reynolds number.
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References
Lerat A., AIAA Paper 83–1925, 1983 or AIAA Journal, 23, 1985, p. 33–40.
Lerat A. and Sides J., in Numerical Methods for Fluid Dynamics III, K.W. Morton and M.J. Baines Eds., Clarendon Press Oxford, 1988, p. 65–86.
Hollanders H., Lerat A. and Peyret R., AIAA Paper 83–1953, 1983 or AIAA journal, 23, 1985, p. 1670–1678.
Khalfallah K. and Lerat A., C. R. Acad. Sc. Paris, 308II, 1989, p. 815–820.
Khalfallah K., Thesis, University Paris V I, October 1990.
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© 1991 Springer-Verlag Berlin Heidelberg
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Khalfallah, K., Lacombe, G., Lerat, A. (1991). Inviscid and Viscous Flow Calculation Over a Double Ellipse with an Implicit Centered Method. 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_37
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DOI: https://doi.org/10.1007/978-3-642-76527-8_37
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-76529-2
Online ISBN: 978-3-642-76527-8
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