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 - Post-Processor
TURBOdesign2 provides a comprehensive post-processor which allows the plotting of the geometry as well as all flow variables in 3D, 2D and 1D.

3D Contours of Pressure Distribution on a transonic fan

2D view of the blade pressure distribution and blade-blade contours

