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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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余西龙 [3]
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Indexed By:EI
Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
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IDDES method based on differential Reynolds-stress model and its application in bluff body turbulent flows
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 119, 页码: 13
Authors:
Wang, Gang
;
Li, Quanzheng
;
Liu Y(刘毅)
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Submit date:2022/06/11
Detached-eddy simulation
Reynolds-stress model
Massively separated flows
Tandem cylinders
Launch vehicle
Transonic buffet
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
Authors:
Yang L(杨磊)
;
Ye, Zhengyin
;
Li WH(李文皓)
;
Sun QH(孙泉华)
Adobe PDF(4621Kb)
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Submit date:2021/11/01
Store separation
Aerodynamic modeling
Interference aerodynamics
Dynamic simulation
Air-launch-to-orbit
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
Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
Authors:
Zhang W
;
Wang S
;
Wang Q
;
Ju SJ(鞠胜军)
;
Yan C
Adobe PDF(2859Kb)
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Submit date:2021/02/09
Aerodynamic thermal
Opposing jets
Parametric sensitivity analysis
Uncertainty quantification
Analysis of Variance
Non-Intrusive Polynomial Chaos
Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(1961Kb)
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Submit date:2020/05/18
Hybrid rocket engine
Paraffin-based fuel
Acrylonitrile-butadiene-styrene
Regression rate
Combustion efficiency
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
Authors:
Wang KL(王宽亮)
;
Li F(李飞)
;
Zou PF(邹鹏飞)
;
Lin X(林鑫)
;
Mao RH(毛荣海)
;
Yu XL(余西龙)
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Adobe PDF(2678Kb)
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View/Download:288/63
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Submit date:2020/03/21
Swirl flame
Heat release
Chemiluminescence
3D-CTC
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
Authors:
Wang KL(王宽亮)
;
Li F(李飞)
;
Zou PF(邹鹏飞)
;
Lin X(林鑫)
;
Mao RH(毛荣海)
;
Yu XL(余西龙)
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  |  
Adobe PDF(2678Kb)
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Submit date:2020/03/21
Swirl flame
Heat release
Chemiluminescence
3D-CTC
An efficient single-loop strategy for reliability-based multidisciplinary design optimization under non-probabilistic set theory
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 148-163
Authors:
Wang XJ
;
Wang RX(王睿星)
;
Wang L
;
Chen XJ
;
Geng XY
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Submit date:2018/10/30
Non-probabilistic reliability based
multidisciplinary design optimization
Single loop strategy
Uncertainty multidisciplinary analysis
Non-probabilistic reliability analysis
Translating distance calculation
Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230
Authors:
Chen XJ
;
Qiu ZP
;
Wang XJ
;
Li YL
;
Wang RX(王睿星)
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Adobe PDF(4860Kb)
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Submit date:2018/02/08
Uncertain Reduced-order Modeling
Robust Flutter Analysis
Interval Perturbation Method
Uncertain Aeroelastic System
An airplane jig shape design method based on high fidelity aeroelastic simulation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 47, 页码: 314-323
Authors:
Yang W
;
Wang QF
;
Zhou L
;
Zheng GN(郑冠男)
;
Liu W
;
Yang, W (reprint author), Commercial Aircraft Corp China Ltd, Beijing Aeronaut Sci & Technol Res Inst, Beijing, Peoples R China.
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Submit date:2016/03/21
Aeroelasticity
Cfd
Csd
Jig Shape
Structural Mesh