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Modeling gasdynamic and heat mass transfer processes in liquid rocket engine of small thrust
N. V. Bezmenovaa, S. A. Shustova, I. E. Ivanovb, U. G. Pirumovb, K. P. Kulyabinc a S. P. Korolyov Samara State Aerospace University
b Moscow Aviation Institute
c Research Institute of Machinery
Abstract:
The program complex for modelling of viscous flows in combustion chamber and nozzles of small
thrust for rocket engines was proposed. Results of numerical investigations for the main characteristics this engine was presented.
Citation:
N. V. Bezmenova, S. A. Shustov, I. E. Ivanov, U. G. Pirumov, K. P. Kulyabin, “Modeling gasdynamic and heat mass transfer processes in liquid rocket engine of small thrust”, Matem. Mod., 13:6 (2001), 5–10
Linking options:
https://www.mathnet.ru/eng/mm722 https://www.mathnet.ru/eng/mm/v13/i6/p5
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Statistics & downloads: |
Abstract page: | 545 | Full-text PDF : | 253 | First page: | 1 |
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