固体推进剂点火准则研究进展OA北大核心CSTPCD
Research Progress in Ignition Criteria of Solid Propellants
为了建立通用的固体推进剂点火准则,分别从实验和模拟两个角度总结了近年来国内外固体推进剂的点火准则.实验层面的点火准则包含判定固体推进剂点火的发火/不发火判据、压力判据、温度判据、光谱辐射强度判据、多参数协同点火判据等.对比分析表明,点火准则均受实验条件以及测试设备的限制,且存在温度等关键点火参数测试难度较大、测试参数延迟等缺陷,因此很难进行拓展应用,但多参数协同的点火判据具有更高的准确性和更大的推广可能性.模拟层面则主要是基于固相、气相、异相点火理论建立的温度点火准则、压力点火准则和化学信号点火准则3类.相较于实验点火准则而言,模拟点火准则更符合固体推进剂的点火理论,但需要从实验获得点火温度、动力学数据等关键参数作为模型输入,且不同种类推进剂的点火理论不尽相同,因此该类点火准则仍需进一步研究.此外,对实验、模拟点火准则进行了关联性和通用性讨论.附参考文献49篇.
In order to establish the general ignition criteria on solid propellant,the recent domestic and foreign solid propellant ignition criteria were summarized from experiment and simulation analysis aspects,respectively.The ignition criteria for solid propellant at the experimental level include ignition/non-ignition criteria,pressure criteria,temperature criteria,spectral radia-tion intensity criteria and multi-parameter co-ignition criteria.Comparative analysis shows that the ignition criteria are limited by the experimental conditions and the test equipments,and there are defects such as the key ignition temperature is difficult to be got,and there is a delay in parameters testing,so it is difficult to expand the application.However,the multi-parameter collaborative ignition criterion has higher accuracy and greater promotion possibility.At the simulation level,the temperature ignition criteria,the pressure ignition criteria and the chemical signal ignition criteria are mainly established based on solid phase,gas phase and out-of-phase ignition theories.Compared with the experimental ignition criterion,the simulated ignition criterion is more consistent with the ignition theory of solid propellant,but the key parameters such as ignition temperature and dynamics data obtained from the experiments are required as the model input,and the ignition theory of different types of pro-pellants is different,so the ignition criterion still needs to be further studied.In addition,the correlation and generality of ex-perimental and simulated ignition criteria are discussed.49 References are attached.
张文科;李泽旭;赵乙丁;刘建忠
浙江大学热能工程研究所,浙江杭州 310027
武器工业
固体推进剂点火准则点火理论研究进展固体火箭发动机
solid propellantignition criterionignition theoryresearch progresssolid rocket motor
《火炸药学报》 2024 (004)
305-315 / 11
评论