Experimental research on aero-propulsion coupling characteristics of a distributed electric propulsion aircraft

Engineering

• Electric Propulsion 100%
• Ducted Fan 75%
• Aerodynamics 50%
• Potential Benefit 50%
• Experimental Result 25%
• Computational Fluid Dynamics 25%
• Wind Tunnel Test 25%
• Angle-of-Attack 25%
• Boundary Layer 25%
• Trailing Edge 25%
• Drag Reduction 25%
• Propulsor 25%
• Interaction Effect 25%
• Electric Motor 25%
• Freestream Flow 25%