Aerodynamic design of wing-body-nacelle-pylon configuration

Engineering

• Aerodynamic Design 100%
• Inboard Wing 100%
• Section Shape 50%
• Lift Coefficient 50%
• Design Result 50%
• Mach Number 50%
• Shock Strength 50%
• Design Objective 50%
• Design Constraint 50%
• Surface Mesh 50%
• Pitch Angle 50%
• Design Iteration 50%
• Objective Function 50%
• Design Optimization 50%
• Drag Coefficient 50%
• Shape Function 50%