CLIPS (Compressible Linear Parabolized Stability) serves to compute boundary-layer flows over turbine blades and swept wings, analyze their stability, and to compute the N factors used in aerodynamic design by using the parabolized stability equations. A graphical user interface provides easy-to-use, selection of data formats and output options, data transfer between tasks, and the choice between interactive mode, control-file generation, or batch mode. As a unique feature, the built-in stability synopsis frees the user from the tedium of finding proper starting data, and allows unattended batch operation from control files. The code has been designed for high efficiency without comprising the quality of the results, and for efficient use by engineers without special training in numerical methods and stability theory.
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.