On the extension of k−ω−SST corrections to predict flow separation on thick airfoils with leading-edge roughness

INIS

• roughness 100%
• corrections 100%
• airfoils 100%
• reynolds number 60%
• shear 60%
• surfaces 40%
• turbulence 40%
• viscosity 40%
• prediction 20%
• boundary layers 20%
• design 20%
• navier-stokes equations 20%
• sensitivity 20%
• pressure coefficient 20%
• distribution 20%
• reduction 20%
• values 20%
• particles 20%
• simulation 20%
• drag coefficient 20%
• lifts 20%
• wind turbines 20%
• pressure gradients 20%
• peaks 20%
• images 20%
• velocity 20%
• errors 20%
• physics 20%
• kinetic energy 20%

Engineering

• Flow Separation 100%
• Thick Airfoil 100%
• Edge Roughness 100%
• Models 33%
• Reynolds Shear Stress 33%
• Turbulence 33%
• Turbulent Kinetic Energy 16%
• Flow Physic 16%
• Pressure Coefficient 16%
• Velocity 16%
• Adverse Pressure Gradient 16%
• Error 16%
• Angle-of-Attack 16%
• Outer Edge 16%
• Outer Region 16%
• Particle Image Velocimetry 16%
• Applicability 16%
• Lift Coefficient 16%
• Blades Design 16%
• High Sensitivity 16%
• Boundary Layer 16%
• Stokes 16%
• Reduction 16%