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Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:  Xing YF(邢云绯);  Zhong FQ(仲峰泉);  Li DX(李东霞);  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(860Kb)  |  Favorite  |  View/Download:451/194  |  Submit date:2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer  
超临界态煤油弯管内湍流流动与对流传热数值研究 会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:  张永江;  仲峰泉;  邢云绯;  张新宇
View  |  Adobe PDF(579Kb)  |  Favorite  |  View/Download:218/53  |  Submit date:2016/08/16
对流传热  湍流流动  弯管  超临界态  低雷诺数流动  对应状态  入口温度  输运特性  传热恶化  二次流动  
超临界态煤油直角弯管内湍流流动与对流传热数值研究 会议论文
中国力学大会-2015, 中国上海, 2015-08-16
Authors:  张永江;  仲峰泉;  邢云绯;  张新宇
View  |  Adobe PDF(229Kb)  |  Favorite  |  View/Download:300/67  |  Submit date:2016/08/16
超临界态  对流传热  湍流流动  方形管  弯管  影响特性  
超临界态煤油冲击射流的数值研究 会议论文
中国力学大会-2015, 中国上海, 2015-08-16
Authors:  邢云绯;  仲峰泉;  张新宇
View  |  Adobe PDF(229Kb)  |  Favorite  |  View/Download:224/60  |  Submit date:2016/08/16
冲击射流  超临界态  冷却结构  航空煤油  离散求解  有限体积法  Stokes  Navier  换热