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 - Competitive Advantage
TURBOdesign2 has been specifically developed for design of highly transonic axial fans where shock/boundary layer interaction has a very significant effect. Its application to the design of these of types of turbomachines can offer many advantages:
- Shorten aerodynamic design times by allowing designers to rapidly optimize the blade surface pressure distributions.
- Allow designers to re-camber the blade profiles with ease in order to achieve a specified pressure ratio or work distribution. This is particularly true in Method 1, where the rVθ distribution is specified.
- Control the 3D pressure field on the rotor.