Geodesic
Modeling gasdynamic and heat mass transfer processes in liquid rocket engine of small thrust
Matematičeskoe modelirovanie, Tome 13 (2001) no. 6, pp. 5-10.

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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. 
@article{MM_2001_13_6_a1,
     author = {N. V. Bezmenova and S. A. Shustov and I. E. Ivanov and U. G. Pirumov and K. P. Kulyabin},
     title = {Modeling gasdynamic and heat mass transfer processes in liquid rocket engine of small thrust},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {5--10},
     publisher = {mathdoc},
     volume = {13},
     number = {6},
     year = {2001},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2001_13_6_a1/}
}
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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. Matematičeskoe modelirovanie, Tome 13 (2001) no. 6, pp. 5-10. http://geodesic.mathdoc.fr/item/MM_2001_13_6_a1/