中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共8条，第1-8条 帮助

限定条件                    
已选(0)清除 条数/页：   排序方式：
Reconciling experimental and theoretical vibrational deactivation in low-energy O + N-2 collisions 期刊论文
PHYSICAL CHEMISTRY CHEMICAL PHYSICS, 2021, 卷号: 23, 期号: 29, 页码: 5
作者:  Hong QZ(洪启臻);  Bartolomei, Massimiliano;  Esposito, Fabrizio;  Coletti, Cecilia;  Sun QH(孙泉华);  Pirani, Fernando
Adobe PDF(3296Kb)  |  收藏  |  浏览/下载：480/96  |  提交时间：2021/08/03
vibronic transition  
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
作者:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  收藏  |  浏览/下载：381/62  |  提交时间：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
作者:  Zhang ZJ(张子健);  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(3599Kb)  |  收藏  |  浏览/下载：328/89  |  提交时间：2021/03/03
Oblique detonation wave  Combustor  Oblique detonation engine  Normal detonation wave  Boundary layer separation  
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
作者:  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)  |  收藏  |  浏览/下载：312/100  |  提交时间：2020/11/30
Quasi-one-dimensional  Detonation  Shock tunnel  Shock speed  
Development of a stagnation streamline model for thermochemical nonequilibrium flow 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 4, 页码: 046102
作者:  Hong QZ(洪启臻);  Wang XY(王小永);  Hu Y(胡远);  Sun QH(孙泉华)
Adobe PDF(2694Kb)  |  收藏  |  浏览/下载：429/117  |  提交时间：2020/04/21
Hypersonic  
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)
Adobe PDF(4374Kb)  |  收藏  |  浏览/下载：393/138  |  提交时间：2019/09/09
Two-phase detonation  CE/SE  Eulerian-Lagrangian  MPI  Aluminum-air detonation  
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
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  
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
作者:  Zhong K;  Yan C;  Chen SS;  Wang XY(王小永);  Ju SJ
Adobe PDF(8635Kb)  |  收藏  |  浏览/下载：214/71  |  提交时间：2019/05/29
Aeroheating  Heatshield configuration  Sphere-cone angle  Mars  Turbulent