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绝热层烧蚀性能的理论预示
引用本文:何国强,陈景蕙.绝热层烧蚀性能的理论预示[J].推进技术,1990,11(4):33-39,77.
作者姓名:何国强  陈景蕙
作者单位:西北工业大学 (何国强),西北工业大学(陈景蕙)
摘    要:本文在多次绝热层烧蚀实验所得物理模型的基础上,建立了在低燃气流速下的烧蚀表面质量和能量控制方程,以及某发动机绝热层在烧蚀时形成的炭化层、热解层和基体的温度响应控制方程,求得了该发动机内弹道环境条件下绝热层烧蚀过程中炭化面和热解面的退移速率.所得数值解与实验结果比较一致.

关 键 词:固体推进剂  火箭发动机  绝热层  烧蚀性能  温度场

A THEORETICAL PREDICTION FOR ABLATION OF LINER INHIBITORS
He Gouqiang and Chen Jinghui.A THEORETICAL PREDICTION FOR ABLATION OF LINER INHIBITORS[J].Journal of Propulsion Technology,1990,11(4):33-39,77.
Authors:He Gouqiang and Chen Jinghui
Institution:Northwestern Polytechnical University
Abstract:On the hasis of many ablation experiments of liner inhibitors,the physical and mathematical model is established. Mass and energy equations at the charring surface, the carbon process layer, the pyrolysis layer and the basis are solved under the condition of low gas velocity. The retreat rates on carbon process face and pyrolysis face and the internal temperature response are obtained under the same condition as in full scale motor.The calculation results are in accordance with ablation experiments adequately.
Keywords:Pocket engine insolutor  Ablation Proporty  Gas analysis  Temperature field  Solid rocket engine
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