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Non-Steady Combustion of Composite Propellants Subjected to Rapid Depressurization 期刊名称： Combustion Science and Technology
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作者： SUHAS, H. K.,BOSE, T. K.
年份： 1982年
teachers期号： 第1-2期
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关键词： Binocular disparity;invariant object recognition;spatial-frequency
analysis;optical flow;Wigner distribution泰语你好
摘要：The aim of the prent work is to carry out parametric analysis of unsteady combustion of composite propellants taking into account all the experimentally obrved phenomena. The theoretical analysis is bad on the time scale analysis of pressure transient, propellant, condend pha reactions, gaspha and ammonium perchlorate particle size. Three influence factors relating to gaspha heat feed back and condend pha energy relea are ud as independently variable paa是什么
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rameters. The influence of each of the influence factors on the predicted dynamic burning rate is found. A mechanism of unsteady combustion of composite propellant subjected to rapid depressurization is postulated. The predicted dynamic burning rates are compared with the available experimental results.
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