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А.В. Алиев, О.В. Мищенкова, И.В. Черепов

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ISSN 0236-3941. Вестник МГТУ им. Н.Э. Баумана. Сер. Машиностроение. 2016. № 4

REFERENCES

[1] Bobylev V.M. Raketnyy dvigatel' tverdogo topliva kak sredstvo upravleniya dvizheniem

raket [The solid propellant rocket engine as a means to control rocket movement]. Moscow,

Mashinostroenie Publ., 1992. 160 p.

[2] Prisnyakov V.F. Dinamika raketnykh dvigateley tverdogo topliva [Dynamics of solid pro-

pellant rocket engines]. Moscow, Mashinostroenie Publ., 1984. 248 p.

[3] Aliev A.V., Mishchenkova O.V. Matematicheskoe modelirovanie v tekhnike [Mathematical

modeling in technology]. Moscow–Izhevsk, Inst. komp'yuternykh issledovaniy Publ., 2012.

476 p.

[4] Zarubin V.S. Matematicheskoe modelirovanie v tekhnike [Mathematical modeling in tech-

nology]. Moscow, MGTU im. N.E. Baumana Publ., 2003. 496 p.

[5] Samarskiy A.A. Mathematical modeling and computer experiment.

Vestn. Akad. Nauk

SSSR

[Herald. Acad. Sci. SSSR], 1979, no. 5, pp. 38–49 (in Russ.).

[6] Solomonov Yu.S., Lipanov A.M., Aliev A.V. Tverdotoplivnye reguliruemye dvigatel'nye

ustanovki. Spravochnaya biblioteka razrabotchika-issledovatelya. T. 9 [Solid propellant adjust-

able propulsion. Reference library of developer and researcher. Vol. 9]. Moscow, Mashi-

nostroenie Publ., 2011. 416 p.

[7] Lipanov A.M., Bobryshev V.P., Aliev A.V. Chislennyy eksperiment v teorii RDTT [Numer-

ical experiment in the theory of solid propellant rocket engines]. Ekaterinburg, Nauka Publ.,

1994. 304 p.

[8] Sorkin R.E. Gazodinamika raketnykh dvigateley na tverdom toplive [Gas dynamics of solid

propellant rocket engines]. Moscow, Nauka Publ., 1967. 368 p.

[9] Besekerskiy V.A., Popov E.P. Teoriya sistem avtomaticheskogo regulirovaniya [The theory

of automatic control systems]. Moscow, Nauka Publ., 1972. 768 p.

[10] Aliev A.V., Blinov D.S. Gas-dynamic problems solutions for irregular shape areas with

application of finite-volume algorithms for large particles method.

Vestnik IzhGTU

[Bulletin

of Kalashnikov ISTU], 2009, no. 1 (41), pp. 151–154 (in Russ.).

[11] Aliev A.V. Paket prikladnykh programm “Tverdotoplivnyy dvigatel'”. Katalog inno-

vatsionnykh razrabotok Izhevskogo gos. tekh. univ. [Software package “Solid propellant rocket

engines”. Catalog of innovative developments of Kalashnikov Izhevsk State Technical Univer-

sity]. Izhevsk, IzhGTU Publ., 2001, p. 24.

[12] Milekhin Yu.M., Klyuchnikov A.N., Fedorychev A.V. Identifikatsiya eksperimental'noy

zavisimosti skorosti goreniya tverdykh topliv ot davleniya. Raketnye dvigateli i problemy

osvoeniya kosmicheskogo prostranstva. T. 1 [Identification of the experimental dependence of

solid propellant combustion rate on the pressure. Rocket engines and challenges of space

exploration. Vol. 1]. Moscow, Torus Press, 2005, pp. 260–262.

[13] Aliev A.V., Mishchenkova O.V., Peremyslovskaya A.G., Cherepova E.V. Identification of

mathematical models of solid-propellant propulsion device with usage of experimental

Results.

Vestnik IzhGTU

[Bulletin of Kalashnikov ISTU], 2008, no. 2, pp. 45–47 (in Russ.).

[14] Zel'dovich Ya.B., Leypunskiy O.I., Librovich V.B. Teoriya nestatsionarnogo goreniya

porokha [The theory of unsteady gunpowder burning]. Moscow, Nauka Publ., 1975. 131 p.

[15] Novozhilov B.V. Nestatsionarnoe gorenie tverdykh raketnykh topliv [Unsteady solid

rocket propellant burning]. Moscow, Nauka Publ., 1973. 176 p.