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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：46/6  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
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：46/0  |  Submit date：2023/04/20
Shock wave  Hypersonic turbulent  boundary layer  Heat transfer  Skin friction decomposition  Direct numerical simulation  
基于主动射流控制的高超声速进气道再起动性能研究（英文） 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:  靳一超;  姚卫
Adobe PDF(1844Kb)  |  Favorite  |  View/Download：164/40  |  Submit date：2023/02/09
高超声速进气道  不起动  再起动  主动射流  流动控制  
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：231/55  |  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)
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Dimple depth  Kerosene  Convective heat transfer  Turbulent flow  
A new dynamic subgrid-scale model using artificial neural network for compressible flow 期刊论文
THEORETICAL AND APPLIED MECHANICS LETTERS, 2022, 卷号: 12, 期号: 4
Authors:  Qi H(齐涵);  Li XL(李新亮);  Luo, Ning;  Yu ZP(于长平)
Adobe PDF(2851Kb)  |  Favorite  |  View/Download：51/12  |  Submit date：2024/01/15
Subgrid-scale kinetic energy  Eddy-viscosity model  Compressible flow  
Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(6382Kb)  |  Favorite  |  View/Download：229/34  |  Submit date：2021/11/01
Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
Adobe PDF(3937Kb)  |  Favorite  |  View/Download：205/52  |  Submit date：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows 期刊论文
ACTA MECHANICA SINICA, 2020, 页码: 9
Authors:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平)
Adobe PDF(2084Kb)  |  Favorite  |  View/Download：354/81  |  Submit date：2020/07/06
Large-eddy simulation  Subgrid-scale model  Rotating turbulent channel flow  
Simulation of shear layers interaction and unsteady evolution under different double backward-facing steps 期刊论文
Theoretical and Applied Mechanics Letters, 2020, 卷号: 10, 页码: 224-229
Authors:  Deng F(邓芳);  Han GL(韩桂来);  Jiang ZL(姜宗林)
Adobe PDF(1546Kb)  |  Favorite  |  View/Download：191/49  |  Submit date：2021/06/11
Interaction  Jet  Numerical simulation  Shear layer  Unsteady evolution