Trim optimizations of an adaptive tailless aircraft with composite wing

Engineering

• Control Surface 100%
• Flaps 50%
• Unmanned Aerial Vehicle 50%
• Genetic Algorithm 50%
• Finite Element Modeling 50%
• Trailing Edge 50%
• Drag Reduction 50%
• Ply Orientation 50%
• Composite Ply 50%
• Induced Drag 50%
• Aeroelastic Tailoring 50%