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Applied Mathematics and Mechanics in Aerospace Industry Read chapter Read first chapter

2021 | OriginalPaper | Chapter

3. Numerical Simulation of Flow Structure Near Descent Module in Mars Atmosphere

Author : Alexander V. Babakov

Published in: Applied Mathematics and Computational Mechanics for Smart Applications

Publisher: Springer Singapore

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Abstract

Based on the conservative numerical method of flux, a hypersonic flow of a viscous heat-conducting gas is simulated near the landing module in Martian atmosphere. Special attention is paid to the study of the structure of non-stationary flow on the side and bottom surfaces of the module. Flow parameters data in the indicated areas are given. Vortex flow patterns near the descent module reflecting the spatial non-stationary nature of the flow are presented. Numerical modeling is implemented on multiprocessor supercomputers of cluster architecture.

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previous chapter Aspects of Meteoroids Flight in the Earth’s Atmosphere
next chapter Mathematical Modeling of Wave Motions of Fluids
Literature
1.
Golomazov, M.M., Finchenko, V.S., Ivankov, A.A., Shmatov, S.I.: Program package for the computer-aided aerodynamic design system for descent vehicles in planetary atmospheres. Sol. Syst. Res. 46(7), 542–547 (2012)CrossRef
2.
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)CrossRef
3.
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)CrossRef
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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)
5.
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)MathSciNetCrossRef
6.
Babakov, A.V., Novikov, P.A.: Numerical simulation of unsteady vortex structures in near wake of poorly streamlined bodies on multiprocessor computer system. Comput. Math. Math. Phys. 51(2), 245–250 (2011)CrossRef
7.
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)CrossRef
Metadata
Title
Numerical Simulation of Flow Structure Near Descent Module in Mars Atmosphere
Author
Alexander V. Babakov
Copyright Year
2021
Publisher
Springer Singapore
Book
Applied Mathematics and Computational Mechanics for Smart Applications

Print ISBN: 978-981-334-825-7

Electronic ISBN: 978-981-334-826-4

Copyright Year: 2021

DOI
https://doi.org/10.1007/978-981-33-4826-4_3

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