Multidisciplinary aerodynamic/structural design optimization for high subsonic transport wing using approximation technique

Engineering

• Aerodynamic Performance 20%
• Aerodynamics 100%
• Aerospace Engineering 20%
• Design Method 20%
• Design Optimization 100%
• Engineering 20%
• Engineering Application 20%
• Equivalent Stress 20%
• Finite Element Analysis 20%
• Kriging Model 60%
• Lift to Drag Ratio 20%
• Multidisciplinary Design Optimization 20%
• Multiobjective Optimization 20%
• Optimisation Problem 20%
• Response Surface Method 80%
• Sample Point 20%
• Structural Design 100%
• Sweep Angle 20%
• Transonic Flow 20%
• Twist Angle 20%