Calculation of Shock Wave Formation in a Shock Tube with a Different Method of Initial Gas Outflow




Calculation of Shock Wave Formation in a
Shock Tube with a Different Method of
Initial Gas Outflow

aerogasodynamics, detonation shock wave.


Volume 24, issue 3, 2023 year


Результаты расчетов распространения детонационных волн в канале с водородосодержащей смесью газов

Приведены результаты расчетов детонационных течений в различных смесях газов, со-держащих H2, O2. Ar. Проведено сравнение с опубликованными теоретическими и экс-периментальными результатами.

аэрогазодинамика, детонационная ударная волна


Volume 24, issue 3, 2023 year



Развитие процесса детонации по времени в канале

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1. A.S. Sokolik Spontaneous ignition and detonation in gases. Moscow: USSR Academy of Sciences 1960. 427 p.
2. M. Netleton. Detonation in gases. Moscow: Mir. 1989. 280 p.
3. Wojciechowski B.V., Mitrofanov V.V., Topchiyan M.E. The structure of the detonation front in gases. Novosibirsk: SB OF the USSR Academy of Sciences. 1960.
4. Zeldovich Ya.B. Theory of detonation propagation in gas systems// ZhETF, 1940, vol. 10, p. 524.
5. Zel’dovich Y.B. Regime classification of an exothermic reaction with nonuniform intial conditions // Combust. Flame. 39. 1980. Р. 211 – 214.
6. Zel’dovich, Ya.B., Librovich V.B., Makhviladze G.M., Sivashinsky, G.I., On the Develop-ment of Detonation in a Nonuniformly Preheated Gas. // Astronautica Acta. 15. 1970. Р.313-320.
7. Chapman D.L. Phil.Mag. 47. 1899. P. 90 – 104.
8. Jouguet E. J. Mathem. Pures Appl. 1. 1905. P. 347 – 425. And2. 1906. P. 542 – 568.
9. Frolov S.M., Zvegintsev V.I., Ivanov V.S. et al. Tests of a model of a detonation ramjet en-gine in a wind tunnel when flowing with an air flow with a Mach number of 5.7 and a braking temperature of 1500 K // Dokl. RAS. 2018. Vol. 481. No. 3. pp. 277-281.
10. A.D. Yegoryan, A.N. Kraiko Comparison of air-jet motors with slow and detonation gorenje // Izvestiya RAS MZhG, 2020, No. 2, pp. 123 -137.
11. Ch. L. Mader Numerical modeling of detonations. Moscow: Mir. 1985. 384 p.
12. Oran E.S., Weber J.W., Stefaniev E.I., Lefebvre M.H. and Anderson J.D. A Numerical Study of a Two-Dimensional H2-O2-Ar Detonation Using a Detailed Chemical Reaction Model // Combustion Flame. 1998. 113. P. 147 – 163.
13. I.A. Kirillov, E.V.Osinina, A.V. Panasenko, M.V. Strelkova //Modelling of formation a deto-nation with use detailedchemical kinetic. Mathematical modeling 2005. V. 17. №11. P. 93 – 102.
14. Marinov N., Westbrook C.K., Pitz W.J. Detailed and global chemical kinetic model for hy-drogen // Transport phenomena in combustion. 1996. V. 1.
15. Mac-Cormak R.W. The effect of viscosity in hypervelocity impact cratering // AIAA Paper 1969-354. 1969. Pp. 69–354