| 超声速地空导弹热环境风洞模拟研究 |
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| 引用本文： | 左应朝.超声速地空导弹热环境风洞模拟研究[J].现代防御技术,2005,33(2):36-39. |
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| 作者姓名： | 左应朝 |
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| 作者单位： | 中国航天科工集团公司,二院二部,北京,100854 |
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| 摘 要： | 根据国内风洞的情况,比较了超声速地空导弹的飞行条件与风洞模拟能力的差距,分析了热环境风洞实验中应采用的相似准则,以及实验数据的处理方法。
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| 关 键 词： | 超声速地空导弹 热环境 风洞模拟 |
| 文章编号： | 1009-086X(2005)02-0036-04 |
| 修稿时间： | 2004年5月18日 |
Wind tunnel simulation research of the thermal environment of supersonic ground to air missile |
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| ZUO Ying-zhao.Wind tunnel simulation research of the thermal environment of supersonic ground to air missile[J].Modern Defence Technology,2005,33(2):36-39. |
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| Authors: | ZUO Ying-zhao |
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| Abstract: | According to the status of domestic wind tunnel,the flight condition of supersonic ground to air missile is compared with the condition that can be simulated by the wind tunnel,the similarity criterion that should be adopted in the thermal environment wind tunnel experiment is analyzed,and the (experimental) data processing is given. |
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| Keywords: | Supersonic ground to air missile Thermal environment Wind tunnel simulation |
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