Optimal hyperelliptic cambered span configurations for minimum drag

Keyphrases

• Hyperelliptic 100%
• Optimization Approach 25%
• Design Optimization 25%
• Design Condition 25%
• Transitional Behavior 25%
• Bending Moment 25%
• Optimization Routine 25%
• Cant 25%
• Flow Features 25%
• Span-wise 25%
• Surface Flow 25%
• Gradient-based Optimization 25%
• Discrete Vortex 25%
• Boundary Layer Transition 25%
• Navier-Stokes Simulation 25%
• Design Configuration 25%
• Fixed Design 25%
• Aerodynamic Drag 25%
• Multidimensional Design 25%
• Lift Coefficient 25%
• Wake Vortex 25%
• Wing Configurations 25%
• Vortex Layer 25%
• Wing Geometry 25%
• Moment Constraints 25%
• Vortex Method 25%
• Camber 25%

Engineering

• Vortex 100%
• Optimal Design 50%
• Optimization Approach 50%
• Design Optimization 50%
• Design Condition 50%
• Bending Moment 50%
• Element Method 50%
• Boundary Layer Transition 50%
• Aerodynamic Drag 50%
• Lift Coefficient 50%
• Fixed Design 50%