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 | 199 | 2011 |
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 | 153 | 2008 |
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 | 104 | 2017 |
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 | 88 | 2018 |
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 | 78 | 2016 |
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 | 70 | 2018 |
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 | 62 | 2019 |
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 | 56 | 2014 |
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 | 47 | 2020 |
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 | 46 | 2022 |
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 | 44 | 2020 |
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 | 38 | 2016 |
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 | 36 | 2016 |
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 | 34 | 2019 |
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 | 34 | 2010 |
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 | 30 | 2018 |
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 | 29 | 2021 |
Evolution of unsteady vortex structures in the tip region of an axial compressor rotor J Hou, Y Liu Physics of Fluids 35 (4), 2023 | 28 | 2023 |
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 | 28 | 2016 |
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 | 28 | 2015 |