Improved aerostructural performance via aeroservoelastic tailoring of a composite wing

Engineering

• Flaps 100%
• Aeroelastic Tailoring 100%
• Trailing Edge 100%
• Thickness Distribution 50%
• Design Solution 50%
• Camber Change 50%
• Aerodynamic Load 50%
• Distributed Control 50%
• Stiffness Distribution 50%
• Optimised Design 50%
• Lift Distribution 50%
• Aircraft Performance 50%
• Control Surfaces 50%
• Structural Property 50%
• Particle Swarm Optimization 50%
• Adaptive Control 50%