MISES©

MISES© is a coupled viscuous/inviscid method for cascade airfoil analysis and design. It consists of menu driven routines which perform functions such as:

Configuration geometric modification.

Gridding of the flowfield.

Subsonic, transonic and supersonic cascade airfoil.

Computational design of cascade airfoils.

Multi-point optimization of cascade airfoils with geometric and aerodynamic constraints.

MISES is based upon a streamline Euler discretization and a two-equation integral boundary layer formation coupled through the displacement thickness and solved simultaneously by a full Newton method.

Frank Dvorak

President