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
Analytical Methods, Inc.
2133 - 152nd Avenue N.E.
Redmond, WA 98052
USA
206-643-9090
206-746-1299 (fax)
frank@amiwest.com
For applications in related solution areas, see the following indices: Aerodynamics, Aerospace, Aircraft Design, Engineering, Gas Turbine Design, Heat/Fluid/Electro-magnetic Flow, Turbo-Machinery Design, the developer index for Analytical Methods, Inc. and the market segment index for Computational Fluid Dynamics (CFD).
MISES is a Copyright of Massachusetts Institute of Technolo
