Aero-propulsive and propulsor cross-coupling effects on a distributed propulsion system

Keyphrases

• Aero 100%
• Propulsor 100%
• Windmilling 100%
• Distributed Propulsion System 100%
• Cross-coupling Effect 100%
• Particle Image Velocimetry 66%
• Velocity Field 66%
• Pressure Distribution 66%
• Airfoil Model 66%
• Nonlinearity 33%
• Airframe 33%
• Trailing Edge 33%
• Wind Tunnel Experiment 33%
• Streamwise 33%
• Three-dimensional Flow 33%
• Characteristic Distribution 33%
• Surface Pressure Distribution 33%
• Fan-out 33%
• Airfoil 33%
• Induced Circulation 33%
• Pitching Moment 33%
• Net Force 33%
• Boundary Layer Height 33%
• Pitching Moment Characteristics 33%
• Circulation Effect 33%
• Ducted Fan 33%
• Thrust Vector 33%
• Boundary Layer Ingestion 33%
• Nonlinear Variation 33%
• Fan Array 33%

Engineering

• Coupling Effect 100%
• Cross-Coupling 100%
• Propulsion System 100%
• Airfoil 100%
• Propulsor 100%
• Particle Image Velocimetry 66%
• Boundary Layer 66%
• Velocity Field 66%
• Pressure Distribution 66%
• Pitching Moment 66%
• Streamwise 33%
• Experimental Result 33%
• Airframe 33%
• Normal Force 33%
• Nonlinearity 33%
• Trailing Edge 33%
• Dimensional Flow 33%
• Moment Characteristic 33%
• Surface Pressure Distribution 33%
• Field Pressure 33%
• Force Model 33%
• Net Force 33%
• Ducted Fan 33%