Selected(0)Clear
Items/Page: Sort: |
| 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 Authors: Wu K(吴坤); Zhang, Peng; Fan XJ(范学军) Adobe PDF(3834Kb)  |  Favorite  |  View/Download:357/57  |  Submit date:2022/01/24 Supersonic combustion Jet-wake flame stabilization Hybrid LES RANS Detailed hydrogen chemistry Counter-rotating vortex pair |
| 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:288/109  |  Submit date:2021/11/01 Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition |
| 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) Adobe PDF(2853Kb)  |  Favorite  |  View/Download:258/74  |  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) Adobe PDF(8067Kb)  |  Favorite  |  View/Download:413/75  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 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) Adobe PDF(2023Kb)  |  Favorite  |  View/Download:342/107  |  Submit date:2020/11/30 Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| 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:291/110  |  Submit date:2020/05/18 Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465 Authors: Wang KL(王宽亮); Li F(李飞); Zou PF(邹鹏飞); Lin X(林鑫); Mao RH(毛荣海); Yu XL(余西龙) View  |  Adobe PDF(2678Kb)  |  Favorite  |  View/Download:282/62  |  Submit date:2020/03/21 Swirl flame Heat release Chemiluminescence 3D-CTC |
| Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465 Authors: Wang KL(王宽亮); Li F(李飞); Zou PF(邹鹏飞); Lin X(林鑫); Mao RH(毛荣海); Yu XL(余西龙) View  |  Adobe PDF(2678Kb)  |  Favorite  |  View/Download:223/73  |  Submit date:2020/03/21 Swirl flame Heat release Chemiluminescence 3D-CTC |
| 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 Authors: Fu YW(符耀威); Yu ZP(于长平); Yan Z(闫正); Li XL(李新亮) View  |  Adobe PDF(2894Kb)  |  Favorite  |  View/Download:408/148  |  Submit date:2020/03/21 Supersonic combustion Turbulence jet Direct numerical simulations Coherent structures |
| Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 92, 页码: 676-684 Authors: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民); Deng, X Adobe PDF(2321Kb)  |  Favorite  |  View/Download:353/87  |  Submit date:2019/10/21 Oblique detonation wave Blunt wedge Initiation Hydrogen |