The predition of aerodynamic characteristics and smart flap of airfoil under the ground effect have been carried out by integatiation of computational fluid dynamics. A parametric bending profile of a smart flap is designed ...

A pressure-based implicit procedure to solve Navier-Stokes equations on a nonorthogonal mesh with collocated finite volume formulation is used to simulate flow around the smart and conventional flaps of spoiler under the ...

In this paper, a pressure-based finite volume procedure is developed in an aerodynamic flow simulation on C- mesh. The boundedness criteria for this procedure are determined from the SBIC, Second and Blending Interpolation ...

A pressure-based implicit procedure to solve Navier-Stokes equations on a nonorthogonal mesh with collocated finite volume formulation is used to simulate flow around the smart and conventional flaps of spoiler under the ...

A pressure-based implicit procedure is due to solve Navier-Stokes

equations. A non-orthogonal mesh with collocated finite volume formulation is

used to simulate flow around the smart and conventional flaps ...