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Self-similar unstart characteristics of supersonic contraction duct with an expansion corner 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 20
Authors:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Wu WN(邬婉楠);  Zhang QF(张启帆);  Chen H(陈昊)
Favorite  |  View/Download：53/0  |  Submit date：2024/03/11
Similarity Analysis on Two-Dimensional Hypersonic Inlets Unstart 期刊论文
AIAA JOURNAL, 2023, 卷号: 61, 期号: 2, 页码: 555-572
Authors:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Chen H(陈昊);  Zhang QF(张启帆);  He CM(何成明)
Adobe PDF(6058Kb)  |  Favorite  |  View/Download：178/50  |  Submit date：2022/11/28
Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass Injection 期刊论文
AIAA JOURNAL, 2022, 页码: 5
Authors:  Li JJ(李江江);  Chen H(陈昊);  Tong XT(仝晓通);  Gao X;  Zhang QF(张启帆);  Yue LJ(岳连捷)
Adobe PDF(1812Kb)  |  Favorite  |  View/Download：235/56  |  Submit date：2022/05/17
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
Authors:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  Favorite  |  View/Download：413/75  |  Submit date：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
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：369/47  |  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