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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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岳连捷 [12]
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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./通讯作者:Yue, Lian-jie
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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View/Download:270/95
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Submit date:2022/11/28
Numerical study on wave configuration of wedge-induced oblique detonation wave: Reactive boundary layer effect
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 11, 页码: 11./通讯作者:Yue, Lianjie
Authors:
Yang L(杨理)
;
Yue LJ(岳连捷)
;
Yu, Dehai
;
Chen, Zheng
Adobe PDF(4548Kb)
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View/Download:273/81
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Submit date:2022/12/29
Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow
期刊论文
AIAA JOURNAL, 2022, 页码: 9./通讯作者:Zhang, Qifan
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)
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View/Download:225/70
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Submit date:2022/07/18
Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor
期刊论文
AIAA JOURNAL, 2022, 页码: 7./通讯作者:Zhang, Qifan, Yue LJ
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)
Adobe PDF(1382Kb)
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View/Download:235/82
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Submit date:2022/03/22
Onset of Oblique Detonation Waves for a Cavity-Based Wedge
期刊论文
AIAA JOURNAL, 2022, 页码: 14
Authors:
Yang, Li
;
Yue LJ(岳连捷)
;
Zhang QF(张启帆)
Adobe PDF(5573Kb)
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View/Download:270/69
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Submit date:2022/03/05
Parameters for evaluating the efficiency of inlet compression
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56./通讯作者:Yue, Lianjie
Authors:
Chen KT(陈科挺)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(511Kb)
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View/Download:338/78
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Submit date:2022/01/12
Airbreathing engine
Compression efficiency
Compression quality
Inlet
Self-consistency
Hysteresis of Shock Train Movement in the Isolator with a Ramp
期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882./通讯作者:Yue, Lianjie
Authors:
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang P
;
Zhao QJ
Adobe PDF(2961Kb)
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View/Download:312/71
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Submit date:2022/02/17
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./通讯作者:Zhang, Qifan
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(8067Kb)
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View/Download:498/105
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188./通讯作者:Yue, Lianjie
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH(马生虎)
;
Zhang QF(张启帆)
;
Zhang, Peng
;
Zhang XY(张新宇)
Adobe PDF(3937Kb)
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View/Download:329/111
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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
Numerical study on the shock/combustion interaction of oblique detonation waves
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13./通讯作者:Yue, Lianjie
Authors:
Yang L
;
Yue LJ(岳连捷)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
Adobe PDF(5176Kb)
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View/Download:419/168
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Submit date:2020/11/30
Oblique detonation wave
Shock/combustion interaction
Shock polar analysis
High-resolution simulation
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