| 注册
首页|期刊导航|航空兵器|气动加热对空空导弹内部电路的温度影响分析

气动加热对空空导弹内部电路的温度影响分析

杨科

航空兵器Issue(1):74-78,5.
航空兵器Issue(1):74-78,5.DOI:10.19297/j.cnki.41-1228/tj.2017.01.012

气动加热对空空导弹内部电路的温度影响分析

Analysis for Temperature Effect of Aerodynamic Heating on the Internal Circuit of the Air-to-Air Missile

杨科1

作者信息

  • 1. 中国空空导弹研究院, 河南 洛阳 471009
  • 折叠

摘要

Abstract

The air-to-air missile subassembly located in special position, cause the harsh operational environment.The temperature effect of the aerodynamic heating to the internal circuit is indicated by this subassembly thermal simulation calculation analysis based on FloTHERM, and the proof for the temperature rise control of the component is carried out.The simulation results show that the temperature rise of the subassembly internal circuit is delayed, and the peak time of shell temperature is the demarcation point where the internal circuit temperature rise changed rapidly, and also more remarkable while the self-flying time is longer.

关键词

热设计/热仿真/气动加热

Key words

thermal design/thermal simulation/aerodynamic heating

分类

信息技术与安全科学

引用本文复制引用

杨科..气动加热对空空导弹内部电路的温度影响分析[J].航空兵器,2017,(1):74-78,5.

航空兵器

OA北大核心CSTPCD

1673-5048

访问量0
|
下载量0
段落导航相关论文