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Intensity Analysis of Base-bleed Device Rocket Assisted Shell

机译:火箭弹辅助炮弹底气强度分析

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Aim Calculate the intensity of base-bleed device rocket. Methods The ANSYS software is used to establish the model of limited units of the increasing distance rocket. The relation of the parts of increasing distance rocket is simulated using touch algorithm. Results The distributing of the body stress under the chamber pressure and lateral pressure can be gained through the analysis of ANSYS. Conclusion The body stress’s dangerous section and its numerical value gained by emulation calculation agree with the ones tested by shooting range. It indicates that the model of limited units and its calculation are right. The method provides design basis for base-bleed device rocket.
机译:目的计算基础排泄装置火箭的强度。方法采用ANSYS软件建立渐进式火箭弹有限单位模型。利用触摸算法模拟了增距火箭各部分之间的关​​系。结果通过ANSYS分析可以得到腔室压力和侧向压力作用下的人体应力分布。结论人体应力的危险区域及其通过仿真计算获得的数值与实测范围内的数值相吻合。这表明有限单位模型及其计算是正确的。该方法为基础排空装置火箭提供了设计依据。

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