侧面燃烧
- 【航天】side burning
侧面燃烧-
采用头部点火设计经验公式对端面-侧面燃烧、尾部点火的小型固体火箭发动机点火药量进行了初步估算。
Based on the experimental formula of fore-ignition design , the initial amorce mass of a small solid rocket motor with end-and-lateral burning grain and aft-ignition manner was estimated firstly .
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对于侧面燃烧装药的固体火箭发动机，在稳定条件下，燃烧室压力-时间曲线上只有少数特殊点处于平衡状态工作，而大量的其它点处于准平衡状态下工作。
In the case of a side-burning grain of a solid propellant rocket engine , only few particular points along the chamber pressure versus time curve under the stable condition are kept in equilibrium . The rest on the curve remain in quasi equilibrium .
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三维侧面突扩燃烧室冷态气流场的数值模拟
Numerical simulation of cold flow field in a three-dimensional side-dump combustor