| 飞行器气动加热环境与结构响应耦合的热结构试验方法 |
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| 引用本文： | 王智勇.飞行器气动加热环境与结构响应耦合的热结构试验方法[J].强度与环境,2006,33(4):59-63. |
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| 作者姓名： | 王智勇 |
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| 作者单位： | 北京强度环境研究所,北京,100076 |
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| 摘 要： | 阐述了将结构热试验和气动加热计算相结合,实现气动热分析与热试验相耦合的试验控制方法。为飞行器的气动加热和结构热响应耦合分析提供了一个解决思路,同时为结构热试验热载荷条件的制定提出了新的方法,对应用复杂防热结构的飞行器的气动热分析和结构热试验具有重要的意义。
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| 关 键 词： | 气动热分析 结构热试验 耦合 |
| 文章编号： | 1006-3919(2006)04-0059-05 |
| 收稿时间： | 2006-07-11 |
| 修稿时间： | 2006-08-03 |
Thermo-structural experiment coupling of aero-heating environment and structural response of aerocraft |
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| WANG Zhi-yong.Thermo-structural experiment coupling of aero-heating environment and structural response of aerocraft[J].Structure & Environment Engineering,2006,33(4):59-63. |
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| Authors: | WANG Zhi-yong |
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| Abstract: | Based on thermo-structural experiment,coupling of aeroheating analysis and thermal test,a new experimental control method is described.It applies a new method for coupling analysis of aeroheating and thermal response,and for instituting heating load conditions of thermo-structural experiment.This method is important to aero-heating analysis and thermo-structural experiment for any aerocraft with duplicate heat insulation structures. |
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| Keywords: | aeroheating analysis thermo-structural experiment coupling |
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