Extension, Validation and Application of the DA VII Transonic Airfoil Code with Passive Shock Control

The contribution of Dasa Airbus (DA) to the EUROSHOCK project within Task 2.1 includes the extension of the DA viscous inviscid interaction transonic airfoil code to passive shock control (SC) by the incorporation of a SC law procedure for the prediction of the ventilation velocity and by the modification of the boundary conditions and of the algebraic eddy viscosity turbulence model for wall mass flow.