Summary
An explicit method of lines approach has been applied for solving hypersonic flows governed by the Euler, Navier-Stokes and Boltzmann equations. The method is based on a finite difference approximation to spatial derivatives and subsequent time integration using the rational Runge-Kutta scheme. Numerical results are presented for the hypersonic flow over a double ellipse which is a test case of the Workshop on Hypersonic Flows for Reentry Problems, January 22–25, 1990 in Antibes(France).
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References
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© 1991 Springer-Verlag Berlin Heidelberg
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Satofuka, N., Morinishi, K. (1991). An Explicit Finite-Difference Solution of Hypersonic Flows Using Rational Runge-Kutta Scheme. 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_41
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DOI: https://doi.org/10.1007/978-3-642-76527-8_41
Publisher Name: Springer, Berlin, Heidelberg
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