nozzle design chart 喷管设计图
nozzle design parameter 喷嘴结构参数
Nozzle reinforcement design 开孔补强结构
design of nozzle 喷头设计
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A new method of the solid propellant rocket nozzle design is presented.
本文介绍一种设计固体火箭喷管的新方法。
Good references for solid rocket motor nozzle design and research are provided.
可为固体火箭发动机喷管的设计与研究提供有效参考。
Several other problems in nozzle design under friction-existing condition are also discussed.
还探讨了摩阻存在条件下喷管投计中的其它几个问题。
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