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This article is cited in 12 scientific papers (total in 12 papers)
Results validation multipurpose software package LOGOS at the decision of problems gasdynamics of start and flight rocets
Yu. N. Deryugina, R. N Zhuchkova, D. K. Zelenskiya, A. S. Kozelkova, A. S. Sarazova, N. F. Kudimovb, Yu. M. Lipnickiyb, A. V. Panasenkob, A. V. Safronovb a FSUE Russian Federal Nuclear Center — All-Russian Research Institute of Experimental Physics, Sarov
b FSUE TsNIIMash, Кorolev
Abstract:
In work possibilities of mathematical modelling of supersonic turbulent streams and a transonic flow by means of software package LOGOS on a basis аverage equations Nave–Stoksa with use of models of turbulence are considered. Results of calculations of not isobaric jet currents and comparison of calculations with experimental data on modes, characteristic for work of impellent installations of rockets of carriers are resulted at start. Results of calculations of a transonic flow of elements rockets and comparison of calculations with experimental data are presented.
Keywords:
Software package LOGOS, gasdynamics start and flight of rockets.
Received: 26.09.2013
Citation:
Yu. N. Deryugin, R. N Zhuchkov, D. K. Zelenskiy, A. S. Kozelkov, A. S. Sarazov, N. F. Kudimov, Yu. M. Lipnickiy, A. V. Panasenko, A. V. Safronov, “Results validation multipurpose software package LOGOS at the decision of problems gasdynamics of start and flight rocets”, Matem. Mod., 26:9 (2014), 83–95; Math. Models Comput. Simul., 7:2 (2015), 144–153
Linking options:
https://www.mathnet.ru/eng/mm3517 https://www.mathnet.ru/eng/mm/v26/i9/p83
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