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Prof. Yangwei LIU (BUAA)
Prof. Yangwei LIU (BUAA)
buaa.edu.cn의 이메일 확인됨
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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
1992011
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
1532008
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
1042017
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
882018
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
702018
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
622019
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
562014
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
472020
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
462022
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
442020
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
382016
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
362016
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
342019
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
342010
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
302018
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
292021
Evolution of unsteady vortex structures in the tip region of an axial compressor rotor
J Hou, Y Liu
Physics of Fluids 35 (4), 2023
282023
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
282016
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
282015
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학술자료 1–20