Optimization and numerical investigation of combined design of blade and endwall on rotor 67

Engineering

• Aerodynamic Performance 100%
• Boundary Layer 50%
• Compressor Rotor 50%
• Dihedral Angle 50%
• Energy Flow 50%
• Freeform Deformation 50%
• NASA 50%
• Pressure Distribution 50%
• Rotors 100%
• Surrogate Model 50%
• Throughflow 50%