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

Keyphrases

• Design Optimization 100%
• Deployable Structures 100%
• High Angle of Attack 100%
• Covert Feathers 100%
• Airfoil 66%
• Design Parameters 33%
• Low Reynolds number 33%
• Evolutionary 33%
• Flap 33%
• Flow Separation 33%
• Spatially Distributed 33%
• UAV 33%
• Covert 33%
• Small Unmanned Air Vehicle 33%
• Deflection Angle 33%
• Structured Systems 33%
• Flap Deflection 33%
• Lift Coefficient 33%
• Covariance Matrix Adaptation Evolution Strategy (CMA-ES) 33%
• Separation Control 33%
• Flap Design 33%
• Discrete Vortex Method 33%
• Stall Mitigation 33%
• Algorithim 33%

Engineering

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