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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:47/1  |  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:87/1  |  提交时间:2023/09/26 Explainability Ensemble Kalman method Turbulence model Axial compressor rotor Neural network Machine learning |
| 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:310/47  |  提交时间:2022/01/24 Supersonic combustion Jet-wake flame stabilization Hybrid LES RANS Detailed hydrogen chemistry Counter-rotating vortex pair |
| 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:380/62  |  提交时间:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10 作者: Ju SJ(鞠胜军); Sun ZX(孙振旭); Yang GW(杨国伟); Prapamonthon P; Zhang JY Adobe PDF(3818Kb)  |  收藏  |  浏览/下载:411/103  |  提交时间:2020/11/30 Optimization design Drag reduction Supersonic flow Energy deposition Opposing jet |
| Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13 作者: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇) Adobe PDF(5176Kb)  |  收藏  |  浏览/下载:255/103  |  提交时间:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10 作者: Zhang X(张旭); Yue LJ(岳连捷); Huang TL(黄庭隆); Zhang QF(张启帆); Zhang XY(张新宇) 浏览  |  Adobe PDF(3862Kb)  |  收藏  |  浏览/下载:332/115  |  提交时间:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 93, 页码: 9 作者: Fu YW(符耀威); Yu ZP(于长平); Yan Z(闫正); Li XL(李新亮) 浏览  |  Adobe PDF(2894Kb)  |  收藏  |  浏览/下载:377/140  |  提交时间:2020/03/21 Supersonic combustion Turbulence jet Direct numerical simulations Coherent structures |
| Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781 作者: Zhong FQ(仲峰泉); Cheng LW(程柳维); Gu HB(顾洪斌); Zhang XY(张新宇) Adobe PDF(2032Kb)  |  收藏  |  浏览/下载:295/86  |  提交时间:2019/05/29 Supersonic combustor Hydrocarbon Mixture fuel Flame structure Ignition |
| 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:369/136  |  提交时间:2018/10/30 Inlet restart Cowl shock Shock wave boundary layer interactions |