文章详细信息 关键词： C/C复合材料;;燃气舵;;数值模拟;;温度场;;热应力 [gap=1045]Keywords: carbon/carbon composites;jet vane;numerical simulation;temperature field;thermal stress
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On the basis of the research of UG further developing skills, author brings forward the master design of jet vane of air-air missile and makes feature model of product by using parameter and feature modeling method and topology structure theory.
本文在UG二次开发研究的基础上,提出燃气舵片模型库总体设计方案,运用参数化设计原理和实体拓扑结构理论,确定参数特征模型,建立和开发了空空导弹燃气舵片模型库系统。
参考来源 - 燃气舵片参数化设计及其软件开发In this paper, the working conditions of rudder in solid rocket motor are investigated detailedly. We computed fluid body around rudder, stress field in the rudder and volumetric ablation of rudder.
本文对固体火箭发动机燃气舵的工作环境进行了系统的研究,计算了燃气舵的流场环境、内部应力场以及热烧蚀情况。
参考来源 - 固体火箭发动机燃气舵热分析研究·2,447,543篇论文数据，部分数据来源于NoteExpress
研究的结论可以为推力矢量发动机及燃气舵的结构设计提供直接的参考。
Therefore, this research would provide a instructive reference straight for the structure design of thrust-vectoring motor and jet et vane.
结合工程实际，论述和分析了推力矢量发动机燃气舵气动特性的设计过程。
The aerodynamics design process of jet vane of the thrust-vector motor is discussed by combining the practical engineering.
采用六分力试验技术对某推力矢量发动机燃气舵的气动特性进行了试验研究。
Computational investigation of secondary flow thrust vector control technology used in a convergent-divergent nozzle;
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