|
Selected(0)Clear
Items/Page: Sort: |
| Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors: Xue R; Zheng X; Yue LJ(岳连捷) ; Zhang SK; Weng C
  Favorite | View/Download：11/0 | Submit date：2020/08/26
Compressible boundary layer combustion Skin-friction reduction Boundary layer transition Transition k-kl-w model Hydrogen combustion |
| Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
Authors: Xue R(薛瑞); Zheng X; Yue LJ(岳连捷); Zhang SK; Weng C
Favorite | View/Download：26/0 | Submit date：2020/07/06
Compressible boundary layer combustion Skin-friction reduction Shock train/flame interaction |
| 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：65/8 | Submit date：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors: Meng Y(孟宇); Gu HB(顾洪斌); Zhuang JH(庄金衡); Sun WM(孙文明); Gao ZB(高占彪); Lian H(连欢); Yue LJ(岳连捷); Chang XY(张新宇)
View | Adobe PDF(3099Kb) | Favorite | View/Download：90/21 | Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| 全流量捕获的高超声速变截面内转式进气道快速设计方法 专利
发明专利. 全流量捕获的高超声速变截面内转式进气道快速设计方法, 专利号: ZL201810269911.2, 申请日期: 2018-03-29,
Inventors: 肖鸿文; 岳连捷; 肖雅彬
View | Adobe PDF(404Kb) | Favorite | View/Download：31/2 | Submit date：2020/02/10 |
| 超燃冲压发动机加速过程中燃烧不稳定性研究 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
Authors: 孟宇; 顾洪斌; 岳连捷; 张新宇
View | Adobe PDF(1057Kb) | Favorite | View/Download：75/16 | Submit date：2019/11/21
超燃冲压发动机 不稳定性 加速过程 直连台 实验研究 |
| Hypergolic ignition modulated by head-on collision, intermixing and convective cooling of binary droplets with varying sizes 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 139, 页码: 475-481
Authors: Zhang DW; Yu DH; Zhang P; Yuan YM(袁越明); Yue LJ(岳连捷); Zhang TC(张泰昌); Fan XJ(范学军)
View | Adobe PDF(1528Kb) | Favorite | View/Download：72/16 | Submit date：2019/09/09 |
| 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：54/5 | Submit date：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| 一种进气道定堵塞度自起动试验装置 专利
发明专利. 一种进气道定堵塞度自起动试验装置, 专利号: ZL201710941567.2, 申请日期: 2017-10-11,
Inventors: 张启帆; 彭辉; 岳连捷; 南轶楠; 张新宇
View | Adobe PDF(502Kb) | Favorite | View/Download：18/0 | Submit date：2020/02/10 |
| 内压缩波系对高超声速进气道自起动性能影响研究 期刊论文
实验流体力学, 2019, 卷号: 33, 期号: 03, 页码: 60-67
Authors: 贾轶楠; 张启帆; 仝晓通; 岳连捷; 张新宇
View | Adobe PDF(2765Kb) | Favorite | View/Download：34/1 | Submit date：2019/09/12
自起动性能 肩部膨胀扇 侧压式 边界层厚度 几何喉道 气动喉道 |
