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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  
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:21/1  |  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  
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
Authors:  Chen H;  Tan H;  Liu YZ;  Zhang QF(张启帆)
Adobe PDF(4679Kb)  |  Favorite  |  View/Download:45/10  |  Submit date:2019/09/09
真实气体效应对Ma10级进气道流动的影响 期刊论文
推进技术, 2019, 卷号: 40, 期号: 05, 页码: 1042-1050
Authors:  张启帆;  岳连捷;  贾轶楠;  张新宇;  李欣;  高雄
Adobe PDF(1675Kb)  |  Favorite  |  View/Download:32/4  |  Submit date:2019/09/12
真实气体效应  高马赫数进气道  化学非平衡气体模型  热完全气体模型  前缘钝化  再起动性能