An automatic differentiation method for uncertainty analysis due to airfoil configuration variation

Engineering

• Aerodynamic Coefficient 50%
• Airfoil 100%
• Computational Fluid Dynamics 50%
• Dynamic Pressure 50%
• Navier-Stokes Equation 50%
• Pressure Coefficient 50%
• Pressure Distribution 50%
• Reynolds-Averaged Navier-Stokes 50%
• Transonic Flow 50%
• Tunnel 50%