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| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors: Lin MY(林明月); Wang C(王春) ; Peng J(彭俊); Jiang ZL(姜宗林)
 Adobe PDF(4805Kb) |  Favorite | View/Download：358/71 | Submit date：2022/01/12 |
| Hysteresis of Shock Train Movement in the Isolator with a Ramp 期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882
Authors: Huang TL(黄庭隆); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang P; Zhao QJ
Adobe PDF(2961Kb) | Favorite | View/Download：248/51 | Submit date：2022/02/17 |
| Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors: Zhou, Lin; Teng, Honghui; Ng, Hoi Dick; Yang PF(杨鹏飞); Jiang ZL(姜宗林)
Adobe PDF(6382Kb) | Favorite | View/Download：256/42 | Submit date：2021/11/01
Cellular detonation Lead shock evolution Multi-layer perceptron Numerical simulations |
| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童)
Adobe PDF(1806Kb) | Favorite | View/Download：307/69 | Submit date：2021/05/17
Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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：282/123 | Submit date：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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)
 View | Adobe PDF(3862Kb) | Favorite | View/Download：371/133 | Submit date：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Investigation on the cycle performance and the combustion characteristic of two CO2-based binary mixtures for the transcritical power cycle 期刊论文
ENERGY, 2019, 卷号: 179, 页码: 454-463
Authors: Pan LS(潘利生); Ma YJ; Li T(李腾); Li HX(李慧鑫); Li B; Wei XL(魏小林)
View | Adobe PDF(1691Kb) | Favorite | View/Download：275/82 | Submit date：2019/09/09
CO2-Based mixtures Transcritical power cycle Waste heat recovery Flammability |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇)
View | Adobe PDF(3918Kb) | Favorite | View/Download：557/183 | Submit date：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| Numerical study of chemically reacting flow in a shock tube using a high-order point-implicit scheme 期刊论文
COMPUTERS & FLUIDS, 2019, 卷号: 184, 页码: 107-118
Authors: Chen S; Sun QH(孙泉华); Klioutchnikov I; Olivier H
View | Adobe PDF(1365Kb) | Favorite | View/Download：352/135 | Submit date：2019/06/10
Shock wave/boundary-layer interactions Real gas effects Chemical nonequilibrium High-order scheme |
| Experimental Investigation on Performance of an Organic Rankine Cycle System Integrated with a Radial Flow Turbine 期刊论文
ENERGIES, 2019, 卷号: 12, 期号: 4, 页码: 20
Authors: Pan LS(潘利生); Wang HX
View | Adobe PDF(4076Kb) | Favorite | View/Download：401/208 | Submit date：2019/05/30
organic Rankine cycle (ORC) system performance radial flow turbine experimental study |
