| 噪声试验技术在高超声速巡航飞行器研制中的应用前景 |
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| 引用本文： | 张卫红,冯秉初,呙道军. 噪声试验技术在高超声速巡航飞行器研制中的应用前景[J]. 强度与环境, 2011, 38(1): 31-35 |
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| 作者姓名： | 张卫红 冯秉初 呙道军 |
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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： | 针对高超声速巡航飞行器的特点,重点对高超声速巡航飞行器特有的声载荷环境下需进行的几项典型噪声试验技术进行阐述,包括试验目的、试验条件和试验方法等.同时列举了各项试验技术在产品研制中的应用实例,概述了相关试验技术在高超声速巡航飞行器研制中的应用前景.
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| 关 键 词： | 高超声速巡航飞行器 噪声试验 振动 |
The advanced research on application of acoustic test technology in developing hypersonic cruise missile |
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| Zhang Weihong,Feng Bingchu,Guo Daojun. The advanced research on application of acoustic test technology in developing hypersonic cruise missile[J]. Structure & Environment Engineering, 2011, 38(1): 31-35 |
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| Authors: | Zhang Weihong Feng Bingchu Guo Daojun |
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| Affiliation: | Zhang Weihong Feng Bingchu Guo Daojun(Beijing Institute of Structure and Environment Engineering,Beijing 100076,China) |
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| Abstract: | In accordance with the characteristics of hypersonic cruise missile,further discussions on some typical acoustic test technologies,including test purpose,test conditions and test procedures,applied to the special acoustic environments of hypersonic cruise missile are given in this paper.Applications of the test technologies in research and development of various kinds of products,and summary of the application vision for hypersonic cruise missile research are also presented. |
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| Keywords: | hypersonic cruise missile acoustic test vibration |
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