TURBOdesign2 - Theory & Flow Model

 

  • Flow solution is provided using cell-vertex, finite volume formulation of the Euler Equations.
  • Equations are solved by Runge-Kutta time marching scheme for asymptotic steady solution with added artificial viscosity (Jameson, 1981).
  • Viscous effects are included using body force method and log law at the walls.
  • Solver is used with normal wall boundary conditions in the case of Method 1.
  • Wall boundary conditions are modified to allow flow transpiration when pressure loading is specified as input (Method 2).