| 巡航导弹防热部件热-振联合试验 |
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| 引用本文： | 吴大方,赵寿根,晏震乾,赵星.巡航导弹防热部件热-振联合试验[J].航空动力学报,2009,24(7):1507-1511. |
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| 作者姓名： | 吴大方 赵寿根 晏震乾 赵星 |
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| 作者单位： | 北京航空航天大学 航空科学与工程学院 固体力学研究所, 北京 100191 |
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| 基金项目： | 凡舟基金(20070506) |
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| 摘 要： | 针对高速巡航导弹防热部件热-振联合试验的需要,建立了高速飞行器高温热-振试验环境模拟系统,该系统由振动激励试验系统和热环境模拟试验系统组成.试验时,热试验系统按照导弹高速飞行过程中弹体表面温度的连续变化对气动加热模拟过程实施动态复现,同时激振系统对防热部件实施振动激励.试验结果表明,该环境试验系统能够为巡航导弹在热振复合状态下的安全飞行提供可靠依据.
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| 关 键 词： | 气动热 隔热 振动试验 巡航导弹 热-振联合试验 |
| 收稿时间： | 2008/12/12 0:00:00 |
| 修稿时间： | 2/12/2009 5:14:14 PM |
Experimental study on thermal-vibration test of thermal insulating component for cruise missile |
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| WU Da-fang,ZHAO Shou-gen,YAN Zhen-qian and ZHAO Xing.Experimental study on thermal-vibration test of thermal insulating component for cruise missile[J].Journal of Aerospace Power,2009,24(7):1507-1511. |
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| Authors: | WU Da-fang ZHAO Shou-gen YAN Zhen-qian and ZHAO Xing |
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| Institution: | Institute of Solid Mechanics, School of Aeronautical Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China |
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| Abstract: | As the need of thermal-vibration composite test for the high-speed vehicle,a thermal-vibration experimental simulation system was established.This experiment system included the vibration experiment system and the thermal experiment system.In the test process,the thermal experiment system simulated the heating process of high-speed cruise by the air,at the same time the vibration experiment system provided the flight vibration environment to the high-speed cruise.The results of the experiment show that this... |
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| Keywords: | aerodynamic heating thermal insulation vibration test cruise missile thermal-vibration test |
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