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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:57/0  |  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)
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Interaction of a shock train with inherent isentropic waves in a curved isolator 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 6, 页码: 21
Authors:  He LH(贺理浩);  Chen H(陈昊);  Yue LJ(岳连捷);  Zhang QF(张启帆);  Wu WN(邬婉楠)
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Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow 期刊论文
AIAA JOURNAL, 2022, 页码: 9
Authors:  Wu ZJ(吴振杰);  Zhang QF(张启帆);  Zhang X(张旭);  Luo WH(罗苇航);  Gao ZB(高占彪);  Yue LJ(岳连捷)
Adobe PDF(3049Kb)  |  Favorite  |  View/Download:169/28  |  Submit date:2022/07/18
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)
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Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor 期刊论文
AIAA JOURNAL, 2022, 页码: 7
Authors:  Zhang X(张旭);  Zhang QF(张启帆);  Wu ZJ(吴振杰);  Yue LJ(岳连捷);  Gao ZB(高占彪);  Luo WH(罗苇航);  Chen H(陈昊)
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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:417/77  |  Submit date:2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow