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The results are better, which show that all portions of propellant are ignited, and the ignition delay is shortened.3.
计算结果比较理想,全部推进剂都被点燃,并且点火延迟时间减小了。
参考来源 - 某旋转固体火箭发动机尾部点火问题的研究·2,447,543篇论文数据,部分数据来源于NoteExpress
改善自发自燃点的柴油燃料,点火延迟时间缩短。
Improves the spontaneous auto-ignition point of diesel fuel, which shortens ignition lag time.
建立了推进器点火过程热传导模型,利用该模型分析了不同因素对点火延迟时问的影响。
A thermal conduct model of ignition phase was established, with which the effect of various parameters on the ignition delay is analyzed.
介绍了基于故障树分析法(FTA)进行的某固体火箭发动机低温下点火延迟故障的分析过程。
The ignition delay fault of solid rocket motor happening in a low temperature based on FTA is analyzed in the paper.
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