COPS

COPS is code for the state-of-the-art analysis of transition in flows over aerodynamic bodies such as swept wings, nacelles, or turbin blades. The code is a full implementation of the compressible nonlinear PSE in general curvilinear coordinates, with interfaces to Navier-Stokes codes and two- and three- dimensional boundary-layer codes. Initial data representative of the disturbance environment in flight, wind tunnels, or gas turbines are selected with the aid of an automated local stability synopsis. COPS then tracks - besides N factors - the transition process downstream, predicting the changes in the skin friction and heat transfer. A Graphical User Interface provides ease of use, an dpost-processing capabilities help interpret and visualize the results.

IRIX version compatibility: 5.2, 5.3, 6.2, 6.3

Thorwald Herbert

President
DYNAFLOW, Inc.
3040 Riverside Drive
Columbus, OH 43221
USA
614-487-9939
614-487-1059 (fax)
Herbert@dynaflow.com

For applications in related solution areas, see the following indices: CFD (Computational Fluid Dynamics), the developer index for DYNAFLOW, Inc. and the product category index for Engineering Analysis.