The Study of Wall Y+ of Incompressible Turbulent Flow Over High Lift Devices Using CutCell Meshing 2013-01-1402
In this study three dimensional numerical simulations were carried out for steady incompressible flows around complex airfoil shapes. NACA-0012 and NACA-23012 wing with 20 percent-c Clark Y flap were used for this study. This work shows that the CutCell mesh method has the ability to generate high quality mesh which captures the details of the viscous boundary layer.
Citation: Ghmati, R., Jawad, B., Liu, L., and Arslan, S., "The Study of Wall Y+ of Incompressible Turbulent Flow Over High Lift Devices Using CutCell Meshing," SAE Technical Paper 2013-01-1402, 2013, https://doi.org/10.4271/2013-01-1402. Download Citation
