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oaioai:dspace.imech.ac.cn:311007/59290

复现高超声速飞行条件下10°尖锥标模气动力特性试验研究

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Publication date
1 January 2015
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Abstract

综述了应用中科院力学所的JF12长试验时间激波风洞中,在复现40km高度,飞行马赫数7的试验条件下,开展的10°尖锥标模天平测力试验研究结果

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Institute Of Mechanics,Chinese Academy of Sciences

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Last time updated on 12/02/2018

This paper was published in Institute Of Mechanics,Chinese Academy of Sciences.

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