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| 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 Authors: Zhai J; Zhang CA(张陈安) ; Wang FM(王发民) ; Zhang WW(张伟为)![](/image/person.jpg)
Adobe PDF(4533Kb)  |   Favorite  |  View/Download:213/58  |  Submit date: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 Authors: Yao W(姚卫) ; Liu H(刘杭); Yue LJ(岳连捷) ; Xiao YB(肖雅彬)![](/image/person.jpg)
Adobe PDF(2954Kb)  |   Favorite  |  View/Download:313/78  |  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)![](/image/person.jpg)
Adobe PDF(4621Kb)  |   Favorite  |  View/Download:308/70  |  Submit date: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 Authors: Xue, Rui; Zheng, Xing; Yue LJ(岳连捷) ; Zhang, Qian; He, Xin; Yang, Jing ; Weng, Chao; Li, Zhihao
Adobe PDF(5483Kb)  |   Favorite  |  View/Download:180/52  |  Submit date: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 Authors: Wang KL(王宽亮) ; Yang PF(杨鹏飞); Teng HH(滕宏辉)![](/image/person.jpg)
Adobe PDF(2853Kb)  |   Favorite  |  View/Download:277/79  |  Submit date: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 Authors: Tong XT(仝晓通) ; Zhang QF(张启帆) ; Yue LJ(岳连捷) ; Zhang XY(张新宇)![](/image/person.jpg)
Adobe PDF(8067Kb)  |   Favorite  |  View/Download:432/84  |  Submit date: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 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)![](/image/person.jpg)
Adobe PDF(2608Kb)  |   Favorite  |  View/Download:283/123  |  Submit date:2020/11/30 Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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 Authors: Luo K(罗凯) ; Wang Q(汪球) ; Li JW(栗继伟); Li JP(李进平) ; Zhao W(赵伟)![](/image/person.jpg)
Adobe PDF(2023Kb)  |   Favorite  |  View/Download:369/113  |  Submit date:2020/11/30 Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8 Authors: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(1657Kb)  |   Favorite  |  View/Download:293/103  |  Submit date:2020/08/26 Scramjet engines Shock-induced combustion ramjet engines Supersonic combustion Chapman-Jouguet detonation |
| 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 Authors: Zhang X(张旭); Yue LJ(岳连捷) ; Huang TL(黄庭隆); Zhang QF(张启帆) ; Zhang XY(张新宇)![](/image/person.jpg)
View  |   Adobe PDF(3862Kb)  |   Favorite  |  View/Download:376/134  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |