Modeling of the plasma environment of re-entry space vehicles

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Shevyrin Alexander A.,Shkredov Timofey Yu.,Shoev Georgy V.,Bondar Yevgeny A.

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Reference22 articles.

1. C. O. Johnston, “Nonequilibrium shock-layer radiative heating for earth and titan entry,” Ph.D. thesis, Faculty of the Virginia Polytechnic Institute and State University 2006.

2. A. Djadkin, A. Beloshitsky, M. Shuvalov, and S. Surzhikov, “Nonequilibrium Radiative Gasdynamics of Segmental-Conical Space Vehicle of Large Size,” in 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA 2011-453, 2011.

3. Development and testing of a numerical simulation method for thermally nonequilibrium dissociating flows in ANSYS Fluent

4. G. Bird, Molecular Gas Dynamics and the Direct Simulation of Gas Flows (Clarendon Press, Oxford, 1994).

5. A. V. Kashkovsky, Y. A. Bondar, G. A. Zhukova, M. S. Ivanov, and S. F. Gimelshein. “ObjectOriented Software Design of Real Gas Effects for the DSMC Method” in 24th International Symposium on Rarefied Gas Dynamics (RGD24), AIP Conference Proceedings 762, edited by M. Capitelli (American Institute of Physics, Melville, NY, 2005), pp. 583–588.

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