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JOURNALS // Matematicheskoe modelirovanie // Archive

Matem. Mod., 2001 Volume 13, Number 6, Pages 5–10 (Mi mm722)

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.



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