IMECH-IR  > 高温气体动力学国家重点实验室
JF-14高温燃气激波管/风洞
董志成
ClassificationJF-14
2000-06-01
Abstract"增加冲压发动机推力研究/高焓流动气动热研究,主要技术指标: 试验段尺寸Φ1.2m, 型面喷管出口尺寸Φ300、500mm Ma数:6~8 总温3000~4500K, 总压5~17 bar 试验时间τ=3~6ms"
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Document Type仪器设备
Identifierhttp://dspace.imech.ac.cn/handle/311007/79594
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
董志成. JF-14高温燃气激波管/风洞(JF-14), 2000.
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