|
已选(0)清除
条数/页： 排序方式： |
| Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor 期刊论文
International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410
作者: Meng Y(孟宇) ; Gu HB(顾洪斌); Zhang XY(张新宇)
 Adobe PDF(3187Kb) |  收藏 | 浏览/下载：215/77 | 提交时间：2021/10/29 |
| 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：380/62 | 提交时间：2021/03/03
Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Ma SH(马生虎); Zhang QF(张启帆); Zhang, Peng; Zhang XY(张新宇)
Adobe PDF(3937Kb) | 收藏 | 浏览/下载：189/45 | 提交时间：2021/03/30
Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| Experimental and numerical investigation on flow and heat transfer of impingement jet cooling of kerosene 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2020, 卷号: 116, 页码: 8
作者: Du MM(杜蒙蒙); Zhong FQ(仲峰泉); Xing YF(邢云绯); Zhang XY(张新宇)
Adobe PDF(2316Kb) | 收藏 | 浏览/下载：263/106 | 提交时间：2020/08/26
Impingement jets Kerosene Heat transfer coefficient Pressure loss Reynolds number |
| 激光诱导荧光聚焦纹影系统及超声速燃烧流场应用 期刊论文
气体物理, 2020, 卷号: 5, 期号: 02, 页码: 14-19
作者: 周芮旭; 连欢; 顾洪斌; 张新宇
 浏览 | Adobe PDF(2073Kb) | 收藏 | 浏览/下载：290/70 | 提交时间：2020/05/06
聚焦纹影 激光诱导荧光 准稳态/非定常 超声速燃烧场 |
| Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
作者: Fan WH(范文慧); Zhong FQ(仲峰泉); Ma SG(马素刚); Zhang XY(张新宇)
浏览 | Adobe PDF(4075Kb) | 收藏 | 浏览/下载：294/86 | 提交时间：2020/03/11
Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| 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)
 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 |
| Numerical Study of Impingement Cooling of Aviation Kerosene at Supercritical Conditions 期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2018, 卷号: 140, 期号: 11, 页码: Ar-112201
作者: Xing YF(邢云绯); Zhong FQ(仲峰泉); Zhang XY(张新宇)
Adobe PDF(2044Kb) | 收藏 | 浏览/下载：300/116 | 提交时间：2018/12/12
impingement cooling supercritical condition heat transfer kerosene |
| Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
作者: Yue LJ(岳连捷); Jia YN(贾轶南); Xu X; Zhang XY(张新宇); Zhang P(张鹏)
Adobe PDF(2110Kb) | 收藏 | 浏览/下载：369/136 | 提交时间：2018/10/30
Inlet restart Cowl shock Shock wave boundary layer interactions |
| The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Jia YN(贾轶南); Yue LJ(岳连捷); Zhang XY(张新宇); Jia, Yinan(yuelj@imech.ac.cn)
Adobe PDF(566Kb) | 收藏 | 浏览/下载：329/72 | 提交时间：2018/01/16
Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
