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Huang Liede (Tong-ji University,Shanghai)
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Abstract: The aim of this article is to consider the mathematical modelsof combustion theory for chemical rocket motors.It includes the followingparts:1.Deflagration-to-detonation transition;2.Spray evaporation;3.Erostive burning of solid rocket moters;4.Stochasic models of fatigue crack propagation;5.The formulation of dynamical equations of motion of complexspacecraft.
Huang Liede (Tong-ji University,Shanghai). SOME MATHEMATICAL MODELS FOR SPACE SCIENCE AND TECHNOLOGY[J]. .
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