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Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences 期刊论文
ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12
Authors:  Lin MY(林明月);  Yang F(杨帆);  Hu ZM(胡宗民);  Han GL(韩桂来)
Favorite  |  View/Download：23/0  |  Submit date：2024/05/27
Shock waves  Shock-shock interaction  Theoretical analysis  Hysteresis  
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  Favorite  |  View/Download：67/10  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
注入光有限相干性对衰荡腔测试方法的影响及求解衰荡时间的强度积分法 期刊论文
物理学报, 2023, 卷号: 72, 期号: 18, 页码: 217-225
Authors:  黄知秋;  张猛;  彭志敏;  王振;  杨乾锁
Adobe PDF(4990Kb)  |  Favorite  |  View/Download：123/25  |  Submit date：2023/11/28
cavity ring-down spectroscopy  light coherence  ring-down time  intensity integration  
Decomposition of mean skin friction in incident shock wave/turbulent boundary layer interaction flows at Mach 2.25 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 9, 页码: 178-194
Authors:  Duan JY(段俊亦);  Tong FL(童福林);  Li XL(李新亮);  Liu HW(刘洪伟)
Adobe PDF(6039Kb)  |  Favorite  |  View/Download：130/9  |  Submit date：2023/11/13
Compressible flow  Boundary layers  Direct numerical simulation  Shock waves  Skin friction  Turbulent flow  
Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:  Yuan CK(苑朝凯);  Meng FZ(孟凡钊);  Liu, Xu;  Liu YF(刘云峰);  Lian H(连欢);  Liu, Yingzheng;  Peng, Di
Adobe PDF(3477Kb)  |  Favorite  |  View/Download：62/7  |  Submit date：2023/07/17
Temperature-sensitive paint  Heat flux  Conjugate gradient method  Air-breathing hypersonic vehicle  Inverse heat conduction problem  
An analytical model for maximum temperature and temperature distribution of plate structure with active cooling 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 5, 页码: 322290
Authors:  Hu GH(胡国豪);  Zhong FQ(仲峰泉);  Chen KT(陈科挺)
Adobe PDF(2013Kb)  |  Favorite  |  View/Download：72/7  |  Submit date：2023/04/20
Plate structure  Active cooling  Thermal protection  Convective heat transfer  Analytical model  
Hypersonic shock wave and turbulent boundary layer interaction in a sharp cone/flare model 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 80-95
Authors:  Tong FL(童福林);  Duan JY(段俊亦);  Lai, Jiang;  Sun, Dong;  Yuan, Xianxu
Adobe PDF(4757Kb)  |  Favorite  |  View/Download：53/2  |  Submit date：2023/04/20
Shock wave  Hypersonic turbulent  boundary layer  Heat transfer  Skin friction decomposition  Direct numerical simulation  
Effect of rib height on turbulent flow and heat transfer of kerosene in rectangular duct 期刊论文
ACTA MECHANICA SINICA, 2022, 卷号: 38, 期号: 7, 页码: 12
Authors:  Li X(李冼);  Zhong FQ(仲峰泉);  Xing YF(邢云绯)
Adobe PDF(5257Kb)  |  Favorite  |  View/Download：249/59  |  Submit date：2022/07/18
Rib height  Kerosene  Heat transfer enhancement  Turbulent flow  
Effect of dimple depth on turbulent flow and heat transfer of kerosene in rectangular duct 期刊论文
ACTA MECHANICA SINICA, 2022, 卷号: 38, 期号: 6, 页码: 12
Authors:  Li X(李冼);  Du MM(杜蒙蒙);  Zhong FQ(仲峰泉)
Adobe PDF(4562Kb)  |  Favorite  |  View/Download：181/27  |  Submit date：2022/07/18
Dimple depth  Kerosene  Convective heat transfer  Turbulent flow  
Oblique detonation wave triggered by a double wedge in hypersonic flow 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184
Authors:  Teng, Honghui;  Zhang, Yuhang;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(1747Kb)  |  Favorite  |  View/Download：199/41  |  Submit date：2022/07/18
Double wedge  Hypersonic flow  Initiation structures  Oblique detonation  Shock interactions