关注
Prof. Yangwei LIU (BUAA)
Prof. Yangwei LIU (BUAA)
在 buaa.edu.cn 的电子邮件经过验证
标题
引用次数
引用次数
年份
Modification of Spalart–Allmaras model with consideration of turbulence energy backscatter using velocity helicity
Y Liu, L Lu, L Fang, F Gao
Physics Letters A 375 (24), 2377-2381, 2011
1852011
Turbulence models assessment for large-scale tip vortices in an axial compressor rotor
Y Liu, X Yu, B Liu
Journal of Propulsion and Power 24 (1), 15-25, 2008
1412008
Investigation of Vortical Structures and Turbulence Characteristics in Corner Separation in a Linear Compressor Cascade Using DDES
Y Liu, H Yan, L Lu, Q Li
Journal of Fluids Engineering 139 (2), 021107, 2017
912017
Turbulence characteristics in corner separation in a highly loaded linear compressor cascade
H Yan, Y Liu, Q Li, L Lu
Aerospace Science and Technology 75, 139-154, 2018
792018
Numerical study of corner separation in a linear compressor cascade using various turbulence models
Y Liu, H Yan, Y Liu, L Lu, Q Li
Chinese Journal of Aeronautics 29 (3), 639-652, 2016
782016
Solidity effect on corner separation and its control in a high-speed low aspect ratio compressor cascade
Y Tang, Y Liu, L Lu
International Journal of Mechanical Sciences 142, 304-321, 2018
602018
Corner separation control by boundary layer suction applied to a highly loaded axial compressor cascade
Y Liu, J Sun, L Lu
Energies 7 (12), 7994-8007, 2014
542014
Comparison of DDES and URANS for unsteady tip leakage flow in an axial compressor rotor
Y Liu, L Zhong, L Lu
Journal of Fluids Engineering 141 (12), 121405, 2019
502019
Passive Separation Control with Blade-End Slots in a Highly Loaded Compressor Cascade
Y Tang, Y Liu, L Lu, H Lu, M Wang
AIAA Journal 58 (1), 85-97, 2020
422020
Modified k-ω model using kinematic vorticity for corner separation in compressor cascades
YW Liu, H Yan, L Fang, LP Lu, QS Li, L Shao
Science China Technological Sciences 59, 795-806, 2016
372016
Effect of vorticity transport on flow structure in the tip region of axial compressors
J Hou, Y Liu, L Zhong, W Zhong, Y Tang
Physics of Fluids 34 (5), 2022
342022
Modification of shear stress transport turbulence model using helicity for predicting corner separation flow in a linear compressor cascade
Y Liu, Y Tang, AD Scillitoe, PG Tucker
Journal of Turbomachinery 142 (2), 021004, 2020
312020
Investigation of unsteady impeller-diffuser interaction in a transonic centrifugal compressor stage
Y Liu, B Liu, L Lu
Turbo Expo: Power for Land, Sea, and Air 44021, 1961-1971, 2010
312010
Effect of Slot at Blade Root on Compressor Cascade Performance under Different Aerodynamic Parameters
Y Liu, J Sun, Y Tang, L Lu
Applied Sciences 6 (12), 421, 2016
302016
Spectral non-equilibrium property in homogeneous isotropic turbulence and its implication in subgrid-scale modeling
L Fang, Y Zhu, Y Liu, L Lu
Physics Letters A 379 (38), 2331-2336, 2015
292015
Evaluation of compressor blading with blade end slots and full-span slots in a highly loaded compressor cascade
Y Tang, Y Liu, L Lu
Journal of Turbomachinery 141 (12), 121002, 2019
272019
Computational model for stall inception and nonlinear evolution in axial flow compressors
Z Xie, Y Liu, X Liu, D Sun, L Lu, X Sun
Journal of Propulsion and Power 34 (3), 720-729, 2018
262018
Numerical study of the effect of secondary vortex on three-dimensional corner separation in a compressor cascade
Y Liu, H Yan, L Lu
International Journal of Turbo & Jet-Engines 33 (1), 9-18, 2016
262016
Study of the Standard k-ε Model for Tip Leakage Flow in an Axial Compressor Rotor
Y Gao, Y Liu, L Zhong, J Hou, L Lu
International Journal of Turbo & Jet-Engines 33 (4), 353–360, 2016
232016
On the relationships between different vortex identification methods based on local trace criterion
Y Liu, W Zhong, Y Tang
Physics of Fluids 33 (10), 2021
222021
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