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This article is cited in 6 scientific papers (total in 6 papers)
Numerical simulation of some problems of recovery capsule aerodynamics
O. M. Belotserkovskya, A. V. Babakova, A. V. Beloshitskiyb, V. I. Gaydaenkoa, A. A. Dyadkinb a Institute for Computer-Aided Design, Russian Academy of Science (ICAD)
b S.P. Korolev Rocket and Space Public Corporation Energia (RSC Energia)
Abstract:
The numerical simulation results of the flow near the recovery capsule with detaching frontal heat shield and jets interaction of the landing multi-nozzles engine with landing field are presented for segment-conical form capsule. The flow structure and the aerodynamic characteristics are studied. The visualization of spatial unsteady vortex structure is implemented. The calculations are based on the unsteady finite-difference schemes of the flux method, approximating the conservation laws in integral form. The numerical simulation is carried out on parallel algorithms and realized on cluster multiprocessor systems.
Keywords:
aerodynamics, recovery capsule, heat shield, landing engine jets, numerical simulations, parallel algorithms, flow visualization.
Received: 29.06.2015
Citation:
O. M. Belotserkovsky, A. V. Babakov, A. V. Beloshitskiy, V. I. Gaydaenko, A. A. Dyadkin, “Numerical simulation of some problems of recovery capsule aerodynamics”, Matem. Mod., 28:2 (2016), 111–122; Math. Models Comput. Simul., 8:5 (2016), 568–576
Linking options:
https://www.mathnet.ru/eng/mm3703 https://www.mathnet.ru/eng/mm/v28/i2/p111
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Abstract page: | 389 | Full-text PDF : | 156 | References: | 61 | First page: | 26 |
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