Aerodynamic Analysis of a Logistics UAV with Foldable Bi-wing Configuration

Engineering

• Aerodynamic Analysis 100%
• Aerodynamic Characteristic 66%
• Aerodynamic Performance 33%
• Airfoil 33%
• Angle-of-Attack 66%
• Axis Angle 33%
• Bypass Flow 33%
• Chord Length 33%
• Design Parameter 33%
• Dimensional Analysis 33%
• Flow Condition 33%
• Flow Field 66%
• Incompressible Flow 33%
• Lift Coefficient 66%
• Two Dimensional 66%
• Unmanned Aerial Vehicle 100%
• Wingspan 33%