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| 超燃冲压发动机加速过程及等离子体对超声速火焰结构的影响 学位论文
博士论文，北京: 中国科学院大学, 2019
作者: 孟宇
 Adobe PDF(11443Kb) |  收藏 | 浏览/下载：682/44 | 提交时间：2019/11/07
超燃冲压发动机，燃烧模态，火焰结构，加速过程，微波，滑移电弧，等离子体 |
| 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：332/115 | 提交时间：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
作者: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良); Jiang ZL(姜宗林)
浏览 | Adobe PDF(4374Kb) | 收藏 | 浏览/下载：392/137 | 提交时间：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
作者: Yang D; Ren JK; Li JW(栗继伟); Wang QL; Wang Q(汪球); Xie Z; Qu XZ
浏览 | Adobe PDF(2608Kb) | 收藏 | 浏览/下载：1024/797 | 提交时间：2019/11/25
Pressure sensitive paint (PSP) Bi-layer structured coating Fast-response Self-referenced measurement |
| 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
作者: Chen H; Tan H; Liu YZ; Zhang QF(张启帆)
浏览 | Adobe PDF(4679Kb) | 收藏 | 浏览/下载：268/97 | 提交时间：2019/09/09 |
| 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
作者: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
浏览 | Adobe PDF(2165Kb) | 收藏 | 浏览/下载：399/93 | 提交时间：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| 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
作者: Deng F(邓放); Han GL(韩桂来); Liu MK(刘美宽); Ding, J; Weng, PF; Jiang ZL(姜宗林)
浏览 | Adobe PDF(5760Kb) | 收藏 | 浏览/下载：542/82 | 提交时间：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
作者: Chen S; Sun QH(孙泉华); Klioutchnikov I; Olivier H
浏览 | Adobe PDF(1365Kb) | 收藏 | 浏览/下载：308/115 | 提交时间：2019/06/10
Shock wave/boundary-layer interactions Real gas effects Chemical nonequilibrium High-order scheme |
| The Role of Three-Dimensional Shock Wave Interaction in the Complex Hypersonic Heating 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者: Wang C(王春); Xiang GX(项高翔); Jiang ZL(姜宗林); Li XD(李旭东); Shi CM(师曾敏)
浏览 | Adobe PDF(376Kb) | 收藏 | 浏览/下载：340/63 | 提交时间：2020/01/06 |
| CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization 期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50
作者: Wang ZP(王知溥); Gu HB(顾洪斌); Cheng L W; Zhong FQ(仲峰泉); Zhang XY(张新宇)
浏览 | Adobe PDF(2630Kb) | 收藏 | 浏览/下载：251/76 | 提交时间：2019/04/11
supersonic combustion one-dimensional modelling heat release CH* chemiluminescence |
