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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 [29]
张新宇 [17]
张启帆 [9]
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Indexed By:EI
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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
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View/Download:44/0
  |  
Submit date:2024/03/11
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:
Dai, Chunliang
;
Sun, Bo
;
Yue LJ(岳连捷)
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yu, Jianyi
Adobe PDF(5674Kb)
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View/Download:54/7
  |  
Submit date:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
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)
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View/Download:161/40
  |  
Submit date:2022/11/28
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)
Adobe PDF(1382Kb)
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View/Download:156/27
  |  
Submit date:2022/03/22
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
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:224/49
  |  
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
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:221/44
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Submit date:2022/02/17
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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View/Download:289/67
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:
Zhou GX(周功喜)
;
Zhang X(张旭)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
;
Lin X(林鑫)
;
Li F(李飞)
;
Chen H(陈宏)
;
Yue LJ(岳连捷)
;
Yu XL(余西龙)
Adobe PDF(4108Kb)
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View/Download:341/51
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Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
Reduction of surface friction drag in scramjet engine by boundary layer combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:
Xue, Rui
;
Zheng, Xing
;
Yue LJ(岳连捷)
;
Zhang, Qian
;
He, Xin
;
Yang, Jing
;
Weng, Chao
;
Li, Zhihao
Adobe PDF(5483Kb)
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View/Download:145/47
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Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
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)
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View/Download:400/69
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow