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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 |
| 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 |
| 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 |
| 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：234/67 | 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 |
| 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
作者: 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) | 收藏 | 浏览/下载：265/110 | 提交时间：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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：254/103 | 提交时间：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
作者: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
Adobe PDF(2023Kb) | 收藏 | 浏览/下载：307/99 | 提交时间：2020/11/30
Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| A multi-time scale solution strategy for an elastomeric aircraft 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 13
作者: Yang L(杨磊); Sun QH(孙泉华)
Adobe PDF(1858Kb) | 收藏 | 浏览/下载：214/89 | 提交时间：2020/08/26
Flight dynamic simulation Multi-time scale Elastomeric aircraft Reduced order models Store separation |
| 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：330/114 | 提交时间：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
