Abstract
For the computation of discontinuities in flow fields which are not fixed beforehand but arise as part of the solution, a large number of methods has been developed. For testing the quality of such methods usually very simple exact solutions are used, e.g. a shock of constant strength running into a gas at rest. Such a test is not rigorous enough because in real problems the functions usually have non-zero derivatives on both sides of the discontinuity. With usual methods it is also difficult to judge the accuracy of numerical solutions near boundaries.
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References
Rusanov, V.V., On difference schemes of third order accuracy for non-linear hyperbolic systems. J.Comp.Phys. 5 (1970) , pp.547–571.
Rusanov, V.V., Advanced techniques for computation of supersonic flow. AIAA-Paper, Annual Conference Jan.1977.
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© 1978 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig
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Rusanov, V.V. (1978). A Test Case for Checking Computational Methods for Gas Flows with Discontinuities. In: Förster, K. (eds) Boundary Algorithms for Multidimensional Inviscid Hyperbolic Flows. Notes on Numerical Fluid Mechanics, vol 1. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-322-85441-4_13
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DOI: https://doi.org/10.1007/978-3-322-85441-4_13
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-528-08075-4
Online ISBN: 978-3-322-85441-4
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