Interaction of oblique deflagration and shock for two-dimensional steady adiabatic combustion system |
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| Authors: | Lijun Pan Xinli Han |
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| Institution: | 1. Department of Mathematics, Nanjing University of Aeronautics and Astronautics, Nanjing, 211106, People’s Republic of China
2. College of Science, Nanjing University of Posts and Telecommunications, Nanjing, 210046, People’s Republic of China
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| Abstract: | The interaction of an oblique deflagration wave and an oblique shock wave for two-dimensional steady adiabatic combustion system is analyzed. Using the shock wave polar and combustion wave polar, we exhibit the construction of the solutions. It is found that the deflagration remains if the shock is weak. However, the shock transforms the deflagration into a detonation(DDT) if it is strong or stops the deflagration if it is proper. |
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