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本文讨论了打开反向喷管时推力终止过程的燃烧室压力衰减和推力瞬变的计算方法。对理论计算与试验结果进行比较,表明经过修正的理论计算结果与试验结果符合得较好。
This article discusses the calculation of the combustion chamber pressure decay and thrust transient at the end of thrust when opening the reverse nozzle. The theoretical calculation and test results are compared, which shows that the corrected theoretical calculation results are in good agreement with the experimental results.