Coupling an inviscid IGA – BEM solver with X-Foil's boundary-layer model for 2D flows

Engineering

• Airfoil 100%
• Algorithm 8%
• Angle-of-Attack 8%
• Boundary Layer 100%
• Computer Aided Design 8%
• Coupled System 16%
• Couplings 100%
• Design System 8%
• Deviation 8%
• Drag Coefficient 8%
• Drag Ratio 8%
• Energy Engineering 8%
• Engineering 8%
• Equation Model 8%
• Flow Model 8%
• Hydrofoil 50%
• Integration 8%
• Kinetic 8%
• Kutta Condition 8%
• Layer Model 100%
• Lift Coefficient 8%
• Lifting Flow 8%
• Low Reynolds Number 16%
• Models 8%
• Optimization 8%
• Pressure Jump 8%
• Shape Optimisation 25%
• Shape Parameter 8%
• Splines 16%
• Trailing Edge 8%
• Velocity Potential 16%

Physics

• Algorithms 8%
• Angle of Attack 8%
• Area 16%
• Boundaries 16%
• Boundary Layer 100%
• Coefficients 8%
• Collocation 8%
• Computer Aided Design 8%
• Correction 8%
• Deviation 8%
• Drag 16%
• Hydrofoils 50%
• Independent Variables 16%
• Integral Equations 16%
• Kinetic Energy 8%
• Low Reynolds Number 16%
• Model 100%
• Momentum 8%
• Optimization 33%
• Output 8%
• Parameter 8%
• Pressure 8%
• Ratios 8%
• Shapes 41%
• Speed 16%
• Systems Engineering 8%
• Transonic Flow 8%