Numerical simulation of some problems of recovery capsule aerodynamics
Matematičeskoe modelirovanie, Tome 28 (2016) no. 2, pp. 111-122

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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.
@article{MM_2016_28_2_a9,
     author = {O. M. Belotserkovsky and A. V. Babakov and A. V. Beloshitskiy and V. I. Gaydaenko and A. A. Dyadkin},
     title = {Numerical simulation of some problems of recovery capsule aerodynamics},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {111--122},
     publisher = {mathdoc},
     volume = {28},
     number = {2},
     year = {2016},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2016_28_2_a9/}
}
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O. M. Belotserkovsky; A. V. Babakov; A. V. Beloshitskiy; V. I. Gaydaenko; A. A. Dyadkin. Numerical simulation of some problems of recovery capsule aerodynamics. Matematičeskoe modelirovanie, Tome 28 (2016) no. 2, pp. 111-122. http://geodesic.mathdoc.fr/item/MM_2016_28_2_a9/