Effects of wavy roughness elements on the aerodynamic performance of NACA0012 airfoil

Engineering

• Aerodynamic Performance 100%
• Airfoil 100%
• Boundary Layer Separation 50%
• Direct Numerical Simulation 50%
• Drag Coefficient 50%
• Flow Structure 25%
• Fourth Order 25%
• Leading Edge 25%
• Lift Coefficient 50%
• Navier-Stokes Equation 25%
• Peak Value 25%
• Roughness Element 100%
• Separation Bubble 50%
• Spanwise Direction 25%
• Streamwise 25%
• Suction Side 25%
• Wave Number 50%

Keyphrases

• Airfoil Aerodynamics 33%
• Massive Separation 33%
• Suction Side 33%
• Surface Roughness Element 33%