Abstract
The numerical simulation of the hypersonic viscous gas flow around the landing module intended for descent in the Martian atmosphere is considered. When modeling the special attention is paid to the study of non-stationary flow structure near the lateral surface and bottom regions of the descent module located at different attack angles. The patterns of the non-stationary spatial vortex flow near the descent module are presented. Numerical simulation is based on the conservative method of finite volumes for the Navier–Stokes model of medium. Numerical simulation is implemented on multiprocessor supercomputers.
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References
Holden, M.S., Wadhams, T.P., MacLean, M., Mundy, E., Parker, R.A.: Experimental studies in LENS I and X to evaluate real gas effects on hypervelocity vehicle performance. In: 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2007–204, pp. 1–17. American Institute of Aeronautics and Astronautics, Reno, Nevada, USA (2007)
Alexashkin, S.N., Martynov, M.B., Pichkhadze, K.M., Finchenko, V.S.: Results of integrated development tests of the Phobos-Grunt spacecraft’s descent module intended to deliver Phobos soil samples to earth. Sol. Syst. Res. 46(7), 502–510 (2012)
Golomazov, M.M., Finchenko, V.S.: Aerodynamic design of a vehicle in the Martian atmosphere under EXOMARS project. Sol. Syst. Res. 48(7), 541–548 (2014)
Finchenko, V.S., Ivankov, A.A., Shmatov, S.I., Mordvinkin, A.S.: Preliminary results of the calculated and experimental studies of the aerothermodynamic parameters of the EXOMARS landing module. Sol. Syst. Res. 49(7), 557–568 (2015)
Belotserkovskii, O.M., Severinov, L.I.: The conservative flow method and the calculation of the flow of a viscous heat-conducting gas past a body of finite size. Comput. Math. Math. Phys. 13(2), 141–156 (1973)
Belotserkovskii, O.M., Babakov, A.V.: The simulation of the coherent vortex structures in the turbulent flows. Adv. Mech. 13(3/4), 135–169 (1990)
Babakov, A.V.: Program package FLUX for the simulation of fundamental and applied problems of fluid dynamics. Comput. Math. Math. Phys. 56(6), 1151–1161 (2016)
Savin, G.I., Shabanov, B.M., Telegin, P.N., Baranov, A.V.: Joint supercomputer center of the Russian academy of sciences: present and future. Lobachevskii J. Math. 40, 1853–1862 (2019)
Babakov, A.V.: Numerical simulation of flow structure near descent module in Mars atmosphere. In: Jain, L.C., Favorskaya, M.N., Nikitin, I.S., Reviznikov, D.L. (eds.) Applied Mathematics and Computational Mechanics for Smart Applications 2020. SIST, vol. 217, pp. 25–34. Springer Nature Singapore Pte Ltd. (2021)
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Calculations were carried out on the computational resources of the Joint Supercomputer Center of the Russian Academy of Sciences (JSCC RAS).
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Babakov, A.V. (2022). Numerical Modeling of Non-stationary Flow Near Lateral Surface of the Descent Module in the Martian Atmosphere for Wide Range of Attack Angles. In: Favorskaya, M.N., Nikitin, I.S., Severina, N.S. (eds) Advances in Theory and Practice of Computational Mechanics. Smart Innovation, Systems and Technologies, vol 274. Springer, Singapore. https://doi.org/10.1007/978-981-16-8926-0_10
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DOI: https://doi.org/10.1007/978-981-16-8926-0_10
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