|
Selected(0)Clear
Items/Page: Sort: |
| 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
Authors: Wang, Gang ; Li, Quanzheng; Liu Y(刘毅)
 Adobe PDF(4661Kb) |  Favorite | View/Download：217/47 | Submit date：2022/06/11
Detached-eddy simulation Reynolds-stress model Massively separated flows Tandem cylinders Launch vehicle Transonic buffet |
| Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors: Li, Mengzhe; Wang, Zhikai; Xu, Rongguang; Zhang, Xiaoliang; Chen, Zhitong; Wang Q(汪球)
Adobe PDF(8841Kb) | Favorite | View/Download：286/109 | Submit date：2021/11/01
Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition |
| 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
Authors: Yao W(姚卫); Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬)
Adobe PDF(2954Kb) | Favorite | View/Download：294/69 | Submit date：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
Authors: Yang L(杨磊); Ye, Zhengyin; Li WH(李文皓); Sun QH(孙泉华)
Adobe PDF(4621Kb) | Favorite | View/Download：284/62 | Submit date：2021/11/01
Store separation Aerodynamic modeling Interference aerodynamics Dynamic simulation Air-launch-to-orbit |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林)
Adobe PDF(2818Kb) | Favorite | View/Download：307/118 | Submit date：2021/01/29
Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
Authors: Zhang W; Wang S; Wang Q; Ju SJ(鞠胜军); Yan C
Adobe PDF(2859Kb) | Favorite | View/Download：278/108 | Submit date：2021/02/09
Aerodynamic thermal Opposing jets Parametric sensitivity analysis Uncertainty quantification Analysis of Variance Non-Intrusive Polynomial Chaos |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(2608Kb) | Favorite | View/Download：274/116 | Submit date：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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
Authors: Ju SJ(鞠胜军); Sun ZX(孙振旭); Yang GW(杨国伟); Prapamonthon P; Zhang JY
Adobe PDF(3818Kb) | Favorite | View/Download：442/113 | Submit date：2020/11/30
Optimization design Drag reduction Supersonic flow Energy deposition Opposing jet |
| Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Yu XL(余西龙)
Adobe PDF(1961Kb) | Favorite | View/Download：289/110 | Submit date：2020/05/18
Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
Authors: Meng BQ(孟宝清); Han GL(韩桂来); Luo ZT(罗长童); Jiang ZL(姜宗林)
Adobe PDF(1937Kb) | Favorite | View/Download：271/88 | Submit date：2018/10/30
Hypersonic Shock tunnel Start-up process Impulse force Vibration |
