... for this oil-cooling issue through various oil-cooler case studies. Premkumar P.S. can be contacted at: premkumar.ps.aeu@kct.ac.in Standard two-equation turbulence models often fail to predict the onset and the amount of flow separation under adverse pressure gradient conditions; henceforth, the shear...

... flow difficult, especially for what concerns the flow separation near the wing leading edge. No transition tripping was used in the wind tunnel model. Without other information, all simulations herein reported were run assuming fully turbulent flow. The one-equation Spalart–Allmaras turbulence model...