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Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
Language:英语
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Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16
Authors:
Chang SY(常思源)
;
Xiao Y(肖尧)
;
Li GL(李广利)
;
Tian ZW(田中伟)
;
Cui K(崔凯)
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View/Download:101/0
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Submit date:2024/01/22
High-pressure capturing wing
Subsonic
Numerical simulation
Wing dihedral
Stability
Numerical study on hypersonic aerodynamic characteristics of the high-pressure capturing wing configuration with wing dihedral
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 15
Authors:
Chang SY(常思源)
;
Xiao Y(肖尧)
;
Li GL(李广利)
;
Tian ZW(田中伟)
;
Cui K(崔凯)
Adobe PDF(8136Kb)
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Submit date:2024/03/11
High-pressure capturing wing
Hypersonic
Numerical simulation
Wing dihedral
Stability
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:
Li, Mengzhe
;
Wang, Zhikai
;
Xu, Rongguang
;
Zhang, Xiaoliang
;
Chen, Zhitong
;
Wang Q(汪球)
Adobe PDF(8841Kb)
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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
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
Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10
Authors:
Ju SJ(鞠胜军)
;
Sun ZX(孙振旭)
;
Yang GW(杨国伟)
;
Prapamonthon P
;
Zhang JY
Adobe PDF(3818Kb)
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Submit date:2020/11/30
Optimization design
Drag reduction
Supersonic flow
Energy deposition
Opposing jet
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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Submit date:2018/02/08
Uncertain Reduced-order Modeling
Robust Flutter Analysis
Interval Perturbation Method
Uncertain Aeroelastic System
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors:
Li HX(李慧鑫)
;
Ye L(叶亮)
;
Wei XL(魏小林)
;
Li T(李腾)
;
Li S(李森)
;
Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2017/12/18
H2o2/kerosene Bipropellant
Coaxial-swirl Injector
Geometric Constant
Performance