Geodesic
Modelling the products of combustion flow in small thrust jet engine nozzles
Matematičeskoe modelirovanie, Tome 11 (1999) no. 6, pp. 45-51.

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The results of solution of determination problem of specific impulse loss because of the chemical non-equilibrium process in nozzles are reported The incomplete flowing of work process in combustion camera for engine thrust 10–2000 H with real fuel components are taking into consideration. 
@article{MM_1999_11_6_a5,
     author = {N. V. Bezmenova and S. A. Shustov and V. Yu. Gidaspov and I. E. Ivanov},
     title = {Modelling the products of combustion flow in small thrust jet engine nozzles},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {45--51},
     publisher = {mathdoc},
     volume = {11},
     number = {6},
     year = {1999},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_1999_11_6_a5/}
}
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N. V. Bezmenova; S. A. Shustov; V. Yu. Gidaspov; I. E. Ivanov. Modelling the products of combustion flow in small thrust jet engine nozzles. Matematičeskoe modelirovanie, Tome 11 (1999) no. 6, pp. 45-51. http://geodesic.mathdoc.fr/item/MM_1999_11_6_a5/