Modeling of reentry space vehicle aerodynamics with control thruster plume — free-stream interaction-Reference-Cited by-同舟云学术

Modeling of reentry space vehicle aerodynamics with control thruster plume — free-stream interaction

Published:2014-12 Issue:6 Volume:21 Page:719-728
ISSN:0869-8643
Container-title:Thermophysics and Aeromechanics
language:en
Short-container-title:Thermophys. Aeromech.

Author:

Kashkovsky A. V.,Vashchenkov P. V.,Banyai T.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Link

http://link.springer.com/content/pdf/10.1134/S0869864314060067.pdf

Reference6 articles.

1. G. Tumino and Y. Gerard, Europe among the world players in atmospheric reentry, ESA Bulletin 128, 2006, P. 62–67.

2. T. Bányai, E. Torres, A.V. Kashkovsky, P.V. Vashchenkov, M.S. Ivanov, and P. Rambaud, Direct Monte Carlo simulations of the intermediate experimental vehicle at early stages of reentry, in: Proc. 7th Aerothermodynamics Symp., 2011, ISBN: 978-92-9221-256-8, P. 425–440.

3. G.A. Bird, Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Clarendon Press, Oxford, 1994.

4. M.S. Ivanov, G.N. Markelov, and S.F. Gimelshein, Statistical simulation of reactive rarefied flows: numerical approach and applications, AIAA Paper, 1998, No. 98-2669.

5. J. Moss, C. Glass, and F. Greene, DSMC simulations of Apollo capsule aerodynamics for hypersonic rarefied conditions, AIAA Paper, 2006, No. 2006-3577.

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