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 - Input Data
- Rotating speed → Specification
- Inlet flow distribution → Specification
- Meridional profile → Assumed based on experience
- Existing Blade shape → Given or can be generated by TurboDesign-1
- Blade number → Assumed based on experience
- Blade thickness → Assumed (structural strength)
- Blade loading → Overview of blade loading
- Stacking condition → Overview of stacking condition