Numerical Simulation of Combustion of a Metallized Composite Solid Propellant with Additives of Nanosized Aluminum Particles

Vasiliy A. Poryazov; Aleksey Yu. Krainov

doi:10.4028/www.scientific.net/KEM.769.346

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Numerical Simulation of Combustion of a Metallized Composite Solid Propellant with Additives of Nanosized Aluminum Particles

Abstract:

The paper presents a numerical simulation of combustion of a metallized composite solid propellant with additives of micron-and nanosized aluminum particles. The model takes into account the thermal effect of decomposition of the condensed phase, convection, diffusion, the exothermic chemical reaction in the gas phase, heating and combustion of aluminum particles in the gas flow, the flow of combustion products, the particle velocity lag relative to the gas. The effect of the Al particle size and mass fraction, emitted from the burning surface, on the burning rate is also taken into consideration.

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High Technology: Research and Applications 2017

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Periodical:

Key Engineering Materials (Volume 769)

Pages:

346-351

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.769.346

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Online since:

April 2018

Authors:

Vasiliy A. Poryazov*, Aleksey Yu. Krainov

Keywords:

Aluminium, Combustion, Mathematical Modeling, Nanosized Particles, Solid Rocket Propellant

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References

[1] L. T. DeLuca, L. Galfetti, F. Severini, L. Meda, G. Marra, A. B. Vorozhtsov, V. S. Sedoi, and V. A. Babuk. Burning of nano-aluminized composite rocket propellants. Comb. Expl. Shock Waves. 41 (2005) 680-692.

DOI: 10.1007/s10573-005-0080-5

Google Scholar

[2] V. A. Arkhipov, A. B. Kiskin, V. E. Zarko, and A. G. Korotkikh. Laboratory method for measurement of the speci¦c impulse of solid propellants. Comb. Expl. Shock Waves 50 (2014) 622-624.

DOI: 10.1134/s0010508214050177

Google Scholar

[3] V. A. Poryazov, A. Y. Krainov, Calculation of the Rate of Combustion of a Metallized Composite Solid Propellant with Allowance for the Size Distribution of Agglomerates. Journal of Engineering Physics and Thermophysics. 89 (3) (2016) 579-586.

DOI: 10.1007/s10891-016-1414-8

Google Scholar

[4] C. E. Hermance, A model of composite propellant combustion including surface heterogeneity and heat generation, AIAA J., 4 (9) (1966) 1629−1637.

DOI: 10.2514/3.55284

Google Scholar

[5] P. F. Pokhil, A. F. Belyaev, Yu. V. Frolov, V. S. Logachev, and A. I. Korotkov, Combustion of Powdered Metals in Active Media[in Russian], Nauka, Moscow (1972).

Google Scholar

[6] D.A. Yagodnikov, Ignition and Combustion of Powdered Metals, Bauman Moscow State Technical University Publishing, Moscow, (2009).

Google Scholar