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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)
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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
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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
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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)
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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)
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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
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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
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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