Benchmarking of Aerodynamic Models for Isolated Propellers Operating at Positive and Negative Thrust

Keyphrases

• Aerodynamic Model 100%
• Maximum Power Output 100%
• Propeller 100%
• Computational Cost 50%
• NavierStokes 50%
• Large Eddy Simulation 50%
• Propeller Performance 50%
• Flow Separation 50%
• Reynolds-averaged 50%
• Lattice Boltzmann 50%
• Lifting Line Theory 25%
• Angle of Attack 25%
• Economic Approach 25%
• Modeling Capability 25%
• Wall Model 25%
• Performance Trends 25%
• Aerodynamics 25%
• Numerical Methods 25%
• Blade Element Momentum Theory 25%
• General Trends 25%
• Comprehensive Assessment 25%
• Flow Effect 25%
• Fidelity Level 25%
• Three-dimensional Flow 25%
• Blade Section 25%

Engineering

• Propeller 100%
• Aerodynamic Model 100%
• Maximum Power Output 80%
• Output Point 80%
• Error 60%
• Accuracy 60%
• Flow Separation 40%
• Performance 40%
• Large Eddy Simulation 40%
• Boltzmann Equation 40%
• Computational Cost 40%
• Conventional Propeller 20%
• Blade Section 20%
• Evaluation 20%
• Aerodynamics 20%
• Aerodynamic Modeling 20%
• Angle-of-Attack 20%
• Numerical Methods 20%
• Lifting Line Theory 20%
• Numerical Analysis 20%
• Mathematical Model 20%
• Dimensional Flow 20%
• Highlight 20%
• Model 20%
• Blade Element Momentum 20%

INIS

• power 100%
• aerodynamics 100%
• output 66%
• errors 50%
• operation 33%
• capture 33%
• reynolds number 33%
• cost 33%
• performance 33%
• large-eddy simulation 33%
• modeling 33%
• levels 16%
• simulation 16%
• comparative evaluations 16%
• assessments 16%
• tools 16%
• walls 16%
• experimental data 16%