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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 [8]
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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)
Adobe PDF(1382Kb)
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Submit date:2022/03/22
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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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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Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
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
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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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
Authors:
Xue R(薛瑞)
;
Zheng X
;
Yue LJ(岳连捷)
;
Zhang SK
;
Weng C
Adobe PDF(3251Kb)
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Submit date:2020/07/06
Compressible boundary layer combustion
Skin-friction reduction
Shock train/flame interaction
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)
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Adobe PDF(3862Kb)
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View/Download:324/112
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration
期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors:
Meng Y(孟宇)
;
Gu HB(顾洪斌)
;
Zhuang JH(庄金衡)
;
Sun WM(孙文明)
;
Gao ZB(高占彪)
;
Lian H(连欢)
;
Yue LJ(岳连捷)
;
Chang XY(张新宇)
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View/Download:357/93
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Submit date:2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration
The vitiation effects of water vapor and carbon dioxide on the autoignition characteristics of kerosene
期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 4, 页码: 485-494
Authors:
Liang JH(梁金虎)
;
Wang S(王苏)
;
Zhang ST(张胜涛)
;
Yue LJ(岳连捷)
;
Fan BC(范秉诚)
;
Zhang XY(张新宇)
;
Cui JP(崔季平)
;
Wang S(王苏)
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View/Download:877/208
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Submit date:2014/08/14
Ignition Delay
Vitiation Effect
Kerosene
Water
Carbon Dioxide
Shock Tube
Chemical kinetics and self-ignition in a model supersonic hydrogen-air combustor
期刊论文
AIAA Journal, 1999, 卷号: 37, 期号: 2, 页码: 208-214
Authors:
Sung CJ
;
Li JG(李建国)
;
Yu G(俞刚)
;
Sung, CJ (reprint author), Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA.
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Submit date:2007/06/15