A generalized hyperbolic marching technique for three-dimensional supersonic flow with shocks-Reference-Cited by-同舟云学术

A generalized hyperbolic marching technique for three-dimensional supersonic flow with shocks

Published: Issue: Volume: Page:341-346
ISSN:
Container-title:Proceedings of the Fourth International Conference on Numerical Methods in Fluid Dynamics
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Author:

Rizzi Arthur W.,Klavins Andrew,MacCormack Robert W.

Publisher

Springer-Verlag

Link

http://link.springer.com/content/pdf/10.1007/BFb0019771.pdf

Reference9 articles.

1. Babenko, K. I., Voskresenskii, G. P., Lyubimov, A. N., and Rusanov, V. V. Prostranstvennoye obtekaniye gladkikh tel ideal'nym gazom. Nauka, Moscow (1964), Engl. Trans. Three-Dimensional Flow of Ideal Gas Past Smooth Bodies. NASA TT F-380 (1966).

2. Chushkin, P. I. Numerical Method of Characteristics for Three-Dimensional Supersonic Flows, in Progress in Aeronautical Sciences (ed. D. Küchemann), vol. 9, Pergamon Press, Oxford (1968).

3. Kutler, P., Reinhardt, W. A., and Warming, R. F. Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas Effects. AIAA J., vol. 11, no. 5, 657–664 (1973).

4. MacCormack, R. W., and Paullay, A. J. Computational Efficiency Achieved by Time Splitting of Finite-Difference Operators. AIAA Paper No. 72–154 (1972).

5. Marconi, F., and Salas, M. Computation of Three-Dimensional Flows About Aircraft Configurations. Computers & Fluids, vol. 1, 185–195 (1973).

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