IMECH-IR  > 高温气体动力学国家重点实验室
JF-8A高超声速激波风洞/炮风洞
吴松
Classification研制
2016
AbstractJF8A为一座激波风洞和自由活塞炮风洞兼用型的脉冲风洞。模拟高超声速准定常流场,可开展高超声速气动力、气动热以及流场显示试验,主要技术指标: 模拟马赫数Ma=6.5~15;模拟单位雷诺数为6E6~4E7/m;试验时间为5ms-30ms;型面喷管出口直径800mm。
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Document Type仪器设备
Identifierhttp://dspace.imech.ac.cn/handle/311007/79581
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
吴松. JF-8A高超声速激波风洞/炮风洞(研制), 2016.
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