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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
作者:
Wu CT(吴楚畋)
;
Wang SZ(王士召)
;
Zhang XL(张鑫磊)
;
He GW(何国威)
收藏
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浏览/下载:15/0
  |  
提交时间:2023/09/26
Explainability
Ensemble Kalman method
Turbulence model
Axial compressor rotor
Neural network
Machine learning
Construction theories of a new type of variable wall thickness scroll profile
期刊论文
Jilin Daxue Xuebao (Gongxueban)/Journal of Jilin University (Engineering and Technology Edition), 2020, 卷号: 50, 期号: 5, 页码: 1627-1634
作者:
Hou, Cai-Sheng
;
Liu, Tao
;
Guo, Li-Xian
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  |  
浏览/下载:13/0
  |  
提交时间:2020/11/14
Geometry
Area utilization
Constructed variable
Geometrical theory
In-depth study
Moving frame
Performance indices
Wall thickness
Working chambers
Leakage Model of Axial Clearance and Test of Scroll Compressors
期刊论文
Journal of Shanghai Jiaotong University (Science), 2020, 卷号: 25, 期号: 4, 页码: 531-537
作者:
Wang, Jianji
;
Liu, Tao
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  |  
浏览/下载:13/0
  |  
提交时间:2020/11/14
Axial-flow compressors
Turbulence models
Axial clearance
Experimental platform
Flow charac-teristics
High-spindle speed
Leakage model
Mass flow rate
Pressure differences
Turbulence theory
Construction and Performance Investigation of Variable Cross-Section Scroll Profiles Based on Frenet Frame
期刊论文
Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2019, 卷号: 53, 期号: 12, 页码: 1495-1501
作者:
Hou, Caisheng
;
Liu, Tao
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  |  
浏览/下载:6/0
  |  
提交时间:2020/11/14
Geometry
Constant cross-section scroll profile
Dynamic performance
Frenet frame
Geometric performance
Variable cross section
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 233, 页码: 5239-5252
作者:
Yang, Chen
;
Wu, Hu
;
Yang, Jinguang
;
Ferlauto, Michele
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浏览/下载:6/0
  |  
提交时间:2019/12/02
Time-marching
throughflow
multistage compressor
blade force
off-design
Calculation of Stall Margin Enhancement With Micro-Tip Injection in an Axial Compressor
期刊论文
Journal of Fluids Engineering, 2019, 卷号: Vol.141 No.8, 页码: 081109
作者:
Xiaohua Liu
;
Jinfang Teng
;
Jun Yang
;
Xiaofeng Sun
;
Dakun Sun
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  |  
浏览/下载:13/0
  |  
提交时间:2019/12/17
Coupling method of stability enhancement based on casing treatments in an axial compressor
期刊论文
2019, 卷号: 95
作者:
Wang, Wei
;
Lu, Jin-ling
;
Luo, Xing-qi
;
Chu, Wu-li
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  |  
浏览/下载:3/0
  |  
提交时间:2019/12/20
Calculation of Stall Margin Enhancement With Micro-Tip Injection in an Axial Compressor
期刊论文
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2019, 卷号: 141
作者:
Liu, Xiaohua
;
Teng, Jinfang
;
Yang, Jun
;
Sun, Xiaofeng
;
Sun, Dakun
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  |  
浏览/下载:18/0
  |  
提交时间:2019/12/30
Axial flow turbomachinery
Axial-flow compressors
Computational fluid dynamics
Eigenvalues and eigenfunctions
Flow fields
Unsteady flow
Computational costs
Computational fluid dynamics simulations
Harmonic decomposition
Homogeneous equations
Linearized navier-stokes equations
Pressure rise coefficient
Qualitative assessments
Unsteady numerical simulations
Navier Stokes equations
An Exponential Decay Model for the Deterministic Correlations in Axial Compressors
期刊论文
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2019, 卷号: 141
作者:
Liu, Yangwei
;
Tang, Yumeng
;
Liu, Baojie
;
Lu, Lipeng
收藏
  |  
浏览/下载:9/0
  |  
提交时间:2019/12/30
Axial flow turbomachinery
Computational fluid dynamics
NASA
Average-passage equation systems
Blade row interaction
Compressor characteristics
Deterministic correlations
Exponential decay models
Multi-stage axial compressors
Multistage compressor
Spanwise distribution
Axial-flow compressors
Analysis and application of shroud wall optimization to an axial compressor with upstream boundary layer to improve aerodynamic performance
期刊论文
INTERNATIONAL JOURNAL OF NUMERICAL METHODS FOR HEAT & FLUID FLOW, 2019, 卷号: 29, 页码: 4237-4261
作者:
Lu, Hanan
;
Li, Qiushi
;
Pan, Tianyu
;
Agarwal, Ramesh
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  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
Aerodynamic performance
Inlet boundary layer
Shroud wall optimization
Transonic compressor rotor
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