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Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows 期刊论文
AIAA JOURNAL, 2018, 卷号: 56, 期号: 8, 页码: 3086-3096
作者:  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1783Kb)  |  收藏  |  浏览/下载:403/125  |  提交时间:2018/10/19
A hybrid kinetic WENO scheme for compressible flow simulations 会议论文
The 10th International Conference on Computational Fluid Dynamics (ICCFD10), Barcelona,Spain, July 9-13, 2018
作者:  Liu HW(刘洪伟);  Yu ZP(于长平);  Li XL(李新亮)
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Gas Kinetic Theory  Numerical Dissipation  Weno Method  Hybrid Numerical Flux  High Order Schemes  
钝头体再入气固热耦合计算方法研究 学位论文
硕士论文,北京: 中国科学院大学, 2018
作者:  田保未
Adobe PDF(4830Kb)  |  收藏  |  浏览/下载:419/12  |  提交时间:2018/05/31
耦合计算  碳基复合材料  烧蚀  网格移动  重映  
Three-dimensional shock wave configurations induced by two asymmetrical intersecting wedges in supersonic flow 期刊论文
SHOCK WAVES, 2018, 卷号: 28, 期号: 2, 页码: 311-319
作者:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
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Supersonic Flow  3d Shock/shock Interaction  3d Asymmetrical Wave Configurations  Spatial Dimension Reduction  
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
作者:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
浏览  |  Adobe PDF(2110Kb)  |  收藏  |  浏览/下载:368/135  |  提交时间:2018/10/30
Inlet restart  Cowl shock  Shock wave boundary layer interactions  
Shock/shock interactions between bodies and wings 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
作者:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1161Kb)  |  收藏  |  浏览/下载:302/74  |  提交时间:2018/10/30
Body And Wing  Flow Field  Hypersonic Flow  Shock/shock Interaction  Wave Configurations