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| Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16
作者: Chang SY(常思源); Xiao Y(肖尧); Li GL(李广利) ; Tian ZW(田中伟); Cui K(崔凯)
  收藏 | 浏览/下载：67/0 | 提交时间：2024/01/22
High-pressure capturing wing Subsonic Numerical simulation Wing dihedral Stability |
| Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18
作者: Guo SQ(郭帅旗); Liu W(刘文); Zhang CA(张陈安); Liu Y(刘洋); Wang FM(王发民)
收藏 | 浏览/下载：23/0 | 提交时间：2024/02/05
Hypersonic waverider Aerodynamic model Symbolic regression Bluntness effect |
| Numerical study on hypersonic aerodynamic characteristics of the high-pressure capturing wing configuration with wing dihedral 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 15
作者: Chang SY(常思源); Xiao Y(肖尧); Li GL(李广利); Tian ZW(田中伟); Cui K(崔凯)
 Adobe PDF(8136Kb) | 收藏 | 浏览/下载：40/2 | 提交时间：2024/03/11
High-pressure capturing wing Hypersonic Numerical simulation Wing dihedral Stability |
| Numerical studies of flow patterns and fuel distribution of tandem-arranged multi jets in a hypersonic crossflow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 139, 页码: 108383
作者: Wang JL(王嘉麟); Han GL(韩桂来)
Adobe PDF(5629Kb) | 收藏 | 浏览/下载：47/0 | 提交时间：2023/07/17
Hypersonic flow Tandem -arranged jets Streamline pattern Vortex structure Fuel -air mixing |
| 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：149/35 | 提交时间：2022/12/20
Shock-wave/boundary-layer interaction Backward-facing step Flow separation Hypersonic inlet |
| 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：262/58 | 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：254/52 | 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：125/42 | 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：235/67 | 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：377/61 | 提交时间：2021/03/03
Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
