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Explainability analysis of neural network-based turbulence modeling for transonic axial compressor rotor flows
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 141, 页码: 108542
Authors:
Wu CT(吴楚畋)
;
Wang SZ(王士召)
;
Zhang XL(张鑫磊)
;
He GW(何国威)
Adobe PDF(3908Kb)
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View/Download:124/11
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Submit date:2023/09/26
Explainability
Ensemble Kalman method
Turbulence model
Axial compressor rotor
Neural network
Machine learning
Three-dimensional flow structures and heat transfer characteristics of compressible flow over a cylindrical cavity
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 122, 页码: 12
Authors:
Wang JT(王江涛)
;
Ma T(马特)
;
Wang Z(王哲)
;
Wang RX(王睿星)
;
Song HW(宋宏伟)
;
Yuan W(袁武)
;
Zheng HW(郑洪伟)
Adobe PDF(4247Kb)
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Submit date:2022/06/10
Cylindrical cavity
Heat transfer
Compressible flow
3D flow behaviors
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
Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 112, 页码: 9
Authors:
Wang KL(王宽亮)
;
Yang PF(杨鹏飞)
;
Teng HH(滕宏辉)
Adobe PDF(2853Kb)
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Submit date:2021/05/17
Oblique detonation
Wave complex
Instability
Thermal choking
Expansion corner
Numerical study on initiation of oblique detonations in hydrogen-air mixtures with various equivalence ratios
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 卷号: 49, 页码: 130-134
Authors:
Zhang YN
;
Gong JS
;
Wang T(王涛)
;
Zhang, YN (reprint author), Beijing Power Machinery Res Inst, State Key Lab Laser Prop & Applicat, Beijing 100074, Peoples R China.
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Submit date:2016/03/21
Detonation
Hydrogen
Initiation
Hypersonic