Geodesic
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. 
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     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},
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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/

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