Publications
- Application of a three-dimensional viscous transonic inverse method to NASA rotor 67
- Development of An (Adaptive) Unstructured 2-D Inverse Design Method for Turbomachinery Blade
- A Viscous Transonic Inverse Design Method for Turbomachinery Blades
- A Three-Dimensional Viscous Transonic Inverse Design Method
- Redesign Of A Transonic Compressor Rotor By Means Of A Three Dimentional Inverse Design Method: A Parametric Study
TURBOdesign2 - CAE Integration
The geometry computed by TURBOdesign2 can be immediately ported to most CAD, CFD and FEA codes. Examples of available general export data formats include IGES, STL, VRML. In addition program specific data export is available for all main CFD codes such as Fluent (G/Turbo), CFX-TURBOgrid, CFX-Bladegen (.rtzt), STAR-CCM+ (es-turbo).


