Verification of a LEWICE-based icing code with coupled heat transfer prediction and aerodynamics performance determination

Engineering

• Aerodynamic Performance 100%
• NASA 100%
• Icing Condition 100%
• Prediction Performance 100%
• Ice Accretion 100%
• Rotor Torque 100%
• Rotors 50%
• Experimental Result 50%
• Experimental Measurement 50%
• Airfoil 50%
• Performance Degradation 50%
• Empirical Model 50%
• Testing Condition 50%
• Degradation Model 50%
• Blade Element Momentum Theory 50%

Keyphrases

• Performance Determination 100%
• Thickness Prediction 66%
• Roughness Transfer 33%
• Prediction Gap 33%
• Fishtail 33%
• Performance Degradation Model 33%
• Ice Shape Prediction 33%