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- W639036826 abstract "A numerical method for the calculation of the incompressible viscous flow at the tip of wings is presented. The method is based on a finite-difference approximation of the Reynolds-averaged Parabolised Navier-Stokes equations for steady incompressible flow. An eddy viscosity algebraic turbulence model is used. The method is applied to the calculation of the flow at the tip of wings with rectangular planform. The sensitivity of the numerical solution to the accuracy of the boundary conditions imposed at the viscous region boundaries is investigated by changing the location of the boundaries. The results show that the method uses an efficient approach to the calculation of tip vortex flows. The specification of the inlet boundary conditions is also investigated and the use of Neumann boundary conditions is proposed to obtain a smoother solution close to the inlet boundary. A good agreement between the numerical predictions and experimental data is obtained. However, the size of the vortex core is overpredicted." @default.
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- W639036826 date "1994-01-01" @default.
- W639036826 modified "2023-09-27" @default.
- W639036826 title "COMPUTATION OF THE TIP VORTEX FLOW ON THREE-DIMENSIONAL FOILS WITH A PARABOLIZED NAVIER-STOKES SOLVER" @default.
- W639036826 hasPublicationYear "1994" @default.
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