Design optimization of a covert feather-inspired deployable structure for increased lift

Engineering

• Angle-of-Attack 100%
• Design Optimization 100%
• Deployable Structure 100%
• Flaps 100%
• Airfoil 66%
• Vortex 33%
• Separation Control 33%
• Flow Separation 33%
• Objective Function 33%
• Covariance Matrix 33%
• Unmanned Aerial Vehicle 33%
• Lift Coefficient 33%
• Design Parameter 33%
• Structure System 33%
• Drone (Aircraft) 33%

Keyphrases

• Discrete Vortex Method 33%
• Flap Design 33%
• Algorithim 33%
• Small Unmanned Air Vehicle 33%