| 高超声速飞行器结构热试验技术进展 |
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| 引用本文： | 张伟,张正平,李海波,孔凡金,吴振强.高超声速飞行器结构热试验技术进展[J].强度与环境,2011,38(1):1-8. |
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| 作者姓名： | 张伟 张正平 李海波 孔凡金 吴振强 |
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| 作者单位： | 北京强度环境研究所可靠性与环境工程技术国防科技重点实验室,北京,100076 |
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| 摘 要： | 重点介绍了美国NASA Dryden飞行研究中心近十年来开展的结构热试验技术研究,包括加热技术、温度测试、热流测试、高温应变测试、传感器安装技术、热结构无损检测等内容,以及进行的高超声速飞行器热结构试验项目.
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| 关 键 词： | 高超声速 热试验 热强度 热结构 |
Progress on thermal test technique of hypersonic vehicle structures |
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| Zhang Wei,Zhang Zhengping,Li Haibo,Kong Fanjin,Wu Zhenqiang.Progress on thermal test technique of hypersonic vehicle structures[J].Structure & Environment Engineering,2011,38(1):1-8. |
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| Authors: | Zhang Wei Zhang Zhengping Li Haibo Kong Fanjin Wu Zhenqiang |
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| Institution: | Zhang Wei Zhang Zhengping Li Haibo Kong Fanjin Wu Zhenqiang (Beijing Institute of Structure and Environment Engineering,Key Laboratory of National Defense Technology for Reliability & Environment Engineering Technology,Beijing 100076,China) |
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| Abstract: | The state of the art of thermal test technique at NASA Dryden Flight Research Center is overviewed,including heating techniques,heat flux measurements,high-temperature strain measurements,sensor attachment techniques,and hot structures non-destructive evaluation and so on.Hot structures test programs of hypersonic vehicle are also presented. |
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| Keywords: | hypersonic thermal test thermal-mechanical hot structure |
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