Selected(0)Clear
Items/Page: Sort: |
| 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:362/127  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework 期刊论文 JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40 Authors: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良) ; Jiang ZL(姜宗林)![](/image/person.jpg)
View  |   Adobe PDF(4374Kb)  |   Favorite  |  View/Download:425/146  |  Submit date:2019/09/09 Two-phase detonation CE/SE Eulerian-Lagrangian MPI Aluminum-air detonation |
| Construction of bi-layer biluminophore fast-responding pressure sensitive coating for non-contact unsteady aerodynamic testing 期刊论文 POLYMER TESTING, 2019, 卷号: 77, 页码: 8 Authors: Yang D; Ren JK; Li JW(栗继伟); Wang QL ; Wang Q(汪球) ; Xie Z; Qu XZ
Adobe PDF(2608Kb)  |   Favorite  |  View/Download:1047/799  |  Submit date:2019/11/25 Pressure sensitive paint (PSP) Bi-layer structured coating Fast-response Self-referenced measurement |
| 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)![](/image/person.jpg)
Adobe PDF(1691Kb)  |   Favorite  |  View/Download:267/80  |  Submit date:2019/09/09 CO2-Based mixtures Transcritical power cycle Waste heat recovery Flammability |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306 Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(2165Kb)  |   Favorite  |  View/Download:423/99  |  Submit date:2019/09/09 Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文 AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523 Authors: Chen H; Tan H; Liu YZ; Zhang QF(张启帆)
Adobe PDF(4679Kb)  |   Favorite  |  View/Download:289/99  |  Submit date:2019/09/09 |
| Numerical simulation of the interaction of two shear layers in double backward-facing steps 期刊论文 PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 5, 页码: 15 Authors: Deng F(邓放); Han GL(韩桂来) ; Liu MK(刘美宽) ; Ding, J; Weng, PF; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(5760Kb)  |   Favorite  |  View/Download:563/91  |  Submit date:2019/10/21 |
| 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
Adobe PDF(1365Kb)  |   Favorite  |  View/Download:341/129  |  Submit date:2019/06/10 Shock wave/boundary-layer interactions Real gas effects Chemical nonequilibrium High-order scheme |
| Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules 期刊论文 ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198 Authors: Zhong K; Yan C; Chen SS; Wang XY(王小永); Ju SJ
View  |   Adobe PDF(8635Kb)  |   Favorite  |  View/Download:248/73  |  Submit date:2019/05/29 Aeroheating Heatshield configuration Sphere-cone angle Mars Turbulent |
| Experimental investigation of liquid film cooling in hypersonic flow 期刊论文 PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10 Authors: Yuan CK(苑朝凯) ; Li JP(李进平) ; Jiang ZL(姜宗林) ; Yu HR(俞鸿儒)![](/image/person.jpg)
View  |   Adobe PDF(4383Kb)  |   Favorite  |  View/Download:460/135  |  Submit date:2019/06/10 |