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高超声速有翼导弹多场耦合动力学的研究和进展(下)
引用本文:杨炳渊,史晓鸣,梁强.高超声速有翼导弹多场耦合动力学的研究和进展(下)[J].强度与环境,2008,35(6).
作者姓名:杨炳渊  史晓鸣  梁强
作者单位:上海航天技术研究院第八设计部,上海,200233
摘    要:在对国内外文献调研的基础上,就有关高超声速有翼导弹多场耦合动力学分析和仿真技术的研究和发展现状进行评述,包括气动加热、大攻角非定常气动力、结构传热和温度场分析、热弹性耦合和热模态分析、耦合动力学分析的数学模型和求解方法等内容。最后针对高超声速有翼导弹提出进一步研究开发的建议。

关 键 词:高超声速  气动加热  模态分析  气动弹性  气动伺服弹性

Investigation and development of the multi-physics coupling dynamics on the hypersonic winged missiles
YANG Bing-yuan,SHI Xiao-ming,LIANG Qiang.Investigation and development of the multi-physics coupling dynamics on the hypersonic winged missiles[J].Structure & Environment Engineering,2008,35(6).
Authors:YANG Bing-yuan  SHI Xiao-ming  LIANG Qiang
Institution:YANG Bing-yuan SHI Xiao-ming LIANG Qiang(The 8th Institute,Shanghai Academy of Spaceflight technology,Shanghai 200233,China)
Abstract:On the basis of studying the intestine and the overseas literatures,the investigation and the development are reviewed of the analysis technology and the simulation technique about the multi-physics coupling dynamics on the hypersonic winged missiles.They includes the aerodynamic heating;the unsteady aerodynamic force with high angle of attack,the analysis of the heat exchange and the temperature field on the structural,the thermo-elasticity coupling and the thermo-modal analysis,the mathematical model and ...
Keywords:hypersonic  aerodynamic heating  modal analysis  aeroelastic  aeroservoelastic  
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