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Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Chen LH(陈立红);  Zhang XY(张新宇);  Xiao YB(肖雅彬)
浏览  |  Adobe PDF(1674Kb)  |  收藏  |  浏览/下载:440/115  |  提交时间:2014/02/24
Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Chang XY(张新宇);  Zhong FQ(仲峰泉)
Adobe PDF(6469Kb)  |  收藏  |  浏览/下载:431/98  |  提交时间:2014/02/24
超临界态煤油圆管湍流的流阻特性研究 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
作者:  党国鑫;  仲峰泉;  陈立红;  张新宇
Adobe PDF(1631Kb)  |  收藏  |  浏览/下载:554/205  |  提交时间:2014/01/23
煤油  超临界  流阻  雷诺相似  数值研究