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1.Hongkai ZHAOorcid_16x16.png, Yangwei LIUorcid_16x16.png, Liang SHAOorcid_16x16.png, Le FANG, Ming DONG (2021).
Existence of positive skewness of velocity gradient in early transition
Phys. Rev. Fluids 6, 104608 (21 pages). doi:10.1103/PhysRevFluids.6.104608 doi.ico hal.ico clarivate_16x16.png
2.Jinjing SUN, Xavier OTTAVYorcid_16x16.png, Yangwei LIUorcid_16x16.png, Lipeng LU (2021).
Corner separation control by optimizing blade end slots in a linear compressor cascade
Aerosp. Sci. Technol. 114, 106737 (14 pages). doi:10.1016/j.ast.2021.106737 doi.ico clarivate_16x16.png
3.Jian FANGorcid_16x16.png, Yanfei GAOorcid_16x16.png, Yangwei LIUorcid_16x16.png, Lipeng LU, Yufeng YAOorcid_16x16.png, Catherine LE RIBAULT (2019).
Direct numerical simulation of a tip-leakage flow in a planar duct with a longitudinal slit
Phys. Fluids 31, 125108 (15 pages). doi:10.1063/1.5124163 doi.ico hal.ico clarivate_16x16.png
4.Feng GAO, Wei MA, Jinjing SUN, Jérôme BOUDETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Yangwei LIUorcid_16x16.png, Lipeng LU, Liang SHAOorcid_16x16.png (2017).
Parameter study on numerical simulation of corner separation in LMFA-NACA65 linear compressor cascade
Chin. J. Aeronauti. 30, 15–30. doi:10.1016/j.cja.2016.09.015 doi.ico hal.ico clarivate_16x16.png
5. Yangwei LIUorcid_16x16.png, Lipeng LU, Le FANG, Feng GAO (2011).
Modification of Spalart?Allmaras model with consideration of turbulence energy backscatter using velocity helicity
Phys. Lett. A 24, 2377–2381. doi:10.1016/j.physleta.2011.05.023 doi.ico clarivate_16x16.png
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