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Physical interpretation of neural network-based nonlinear eddy viscosity models 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 142, 页码: 13
作者:  Zhang XL(张鑫磊);  Xiao, Heng;  Jee, Solkeun;  He GW(何国威)
Adobe PDF(5699Kb)  |  收藏  |  浏览/下载：52/1  |  提交时间：2023/11/28
Machine learning  Turbulence modeling  Ensemble Kalman inversion  Physical interpretability  
Explainability analysis of neural network-based turbulence modeling for transonic axial compressor rotor flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 141, 页码: 108542
作者:  Wu CT(吴楚畋);  Wang SZ(王士召);  Zhang XL(张鑫磊);  He GW(何国威)
Adobe PDF(3908Kb)  |  收藏  |  浏览/下载：98/6  |  提交时间：2023/09/26
Explainability  Ensemble Kalman method  Turbulence model  Axial compressor rotor  Neural network  Machine learning  
Control of shock-wave/boundary-layer interaction using abackward-facing step 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 126, 页码: 13
作者:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW(张伟为)
Adobe PDF(4533Kb)  |  收藏  |  浏览/下载：164/40  |  提交时间：2022/12/20
Shock-wave/boundary-layer interaction  Backward-facing step  Flow separation  Hypersonic inlet  
On jet-wake flame stabilization in scramjet: A LES/RANS study from chemical kinetic and fluid-dynamical perspectives 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 120, 页码: 12
作者:  Wu K(吴坤);  Zhang, Peng;  Fan XJ(范学军)
Adobe PDF(3834Kb)  |  收藏  |  浏览/下载：325/51  |  提交时间：2022/01/24
Supersonic combustion  Jet-wake flame stabilization  Hybrid LES  RANS  Detailed hydrogen chemistry  Counter-rotating vortex pair  
IDDES method based on differential Reynolds-stress model and its application in bluff body turbulent flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 119, 页码: 13
作者:  Wang, Gang;  Li, Quanzheng;  Liu Y(刘毅)
Adobe PDF(4661Kb)  |  收藏  |  浏览/下载：198/41  |  提交时间：2022/06/11
Detached-eddy simulation  Reynolds-stress model  Massively separated flows  Tandem cylinders  Launch vehicle  Transonic buffet  
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
作者:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
Adobe PDF(2954Kb)  |  收藏  |  浏览/下载：281/64  |  提交时间：2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
作者:  Yang L(杨磊);  Ye, Zhengyin;  Li WH(李文皓);  Sun QH(孙泉华)
Adobe PDF(4621Kb)  |  收藏  |  浏览/下载：269/57  |  提交时间：2021/11/01
Store separation  Aerodynamic modeling  Interference aerodynamics  Dynamic simulation  Air-launch-to-orbit  
Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
作者:  Xue, Rui;  Zheng, Xing;  Yue LJ(岳连捷);  Zhang, Qian;  He, Xin;  Yang, Jing;  Weng, Chao;  Li, Zhihao
Adobe PDF(5483Kb)  |  收藏  |  浏览/下载：133/46  |  提交时间：2022/10/25
Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine  
Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 112, 页码: 9
作者:  Wang KL(王宽亮);  Yang PF(杨鹏飞);  Teng HH(滕宏辉)
Adobe PDF(2853Kb)  |  收藏  |  浏览/下载：244/69  |  提交时间：2021/05/17
Oblique detonation  Wave complex  Instability  Thermal choking  Expansion corner  
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
作者:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  收藏  |  浏览/下载：391/67  |  提交时间：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow