Two-dimensional numerical simulation of ablative thermal insulators in solid rocket motor combustion chamber

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Razmjooei Mohammad; OMMI FATHOLLAH; SHAHBAZI MOHAMMAD

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Journal: Journal of Space Science and Technology Year:2020 | Volume:13 | Issue:2 (43) Page(s): 13-34

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Information Journal Paper

Title

Two-dimensional numerical simulation of ablative thermal insulators in solid rocket motor combustion chamber

Author(s)

Razmjooei Mohammad | OMMI FATHOLLAH | SHAHBAZI MOHAMMAD | Issue Writer Certificate

Keywords

AblationQ1

InsulatorsQ1

Finite volumeQ2

Two-dimensionalQ1

heat transferQ2

Decomposition equationQ1

Abstract

In this paper, the heat transfer and Ablation thermal Insulators in solid rocket motor are investigated. Therefore, by collecting and solving the thermal Ablation equations, a computer program, using MATLAB software, is developed which can predict the thermal response of Insulators in different operating conditions and compare the performance of these Insulators. The heat and mass transfer equations are considered in two dimensions in a solid body. We used the equations, Finite volume method with implicit formulation for time dependency to solve equations. The reaction equation which written in the form of Arrhenius, is solved using Runge-Kutta method, and the density and the flux of the gas produced at each step are obtained. Also we represent a model for the rate of recession.

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APA: Copy

Razmjooei, Mohammad, OMMI, FATHOLLAH, & SHAHBAZI, MOHAMMAD. (2020). Two-dimensional numerical simulation of ablative thermal insulators in solid rocket motor combustion chamber. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 13(2 (43) ), 13-34. SID. https://sid.ir/paper/389895/en

Vancouver: Copy

Razmjooei Mohammad, OMMI FATHOLLAH, SHAHBAZI MOHAMMAD. Two-dimensional numerical simulation of ablative thermal insulators in solid rocket motor combustion chamber. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2020;13(2 (43) ):13-34. Available from: https://sid.ir/paper/389895/en

IEEE: Copy

Mohammad Razmjooei, FATHOLLAH OMMI, and MOHAMMAD SHAHBAZI, “Two-dimensional numerical simulation of ablative thermal insulators in solid rocket motor combustion chamber,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 13, no. 2 (43) , pp. 13–34, 2020, [Online]. Available: https://sid.ir/paper/389895/en

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