Experimental study on the wing-wake interaction of a flapping wing Micro Aerial Vehicle

Keyphrases

• Wing-wake Interaction 100%
• Flapping-wing Micro Aerial Vehicles (FWMAVs) 100%
• Particle Image Velocimetry 66%
• Clapping 66%
• Camber 66%
• Energy Efficiency 33%
• High Power 33%
• Oil Droplet 33%
• Relative Location 33%
• Power Efficiency 33%
• Flow Field 33%
• Rhodamine B (Rh B) 33%
• Power Generation Efficiency 33%
• Force Measurement 33%
• Fluorescent Particles 33%
• Hovering 33%
• Leading Edge Vortex 33%
• Optical Filters 33%
• Force Generation 33%
• Camera Lens 33%
• Aerodynamics 33%
• Deformation Characteristics 33%
• Relative Strength 33%
• Stiffener 33%
• Vehicle Platform 33%
• Motion Flow 33%
• Lift Force 33%
• Motion Capture Measurement 33%
• Carbon Fiber Rod 33%
• Fixed Position 33%
• Fog Droplets 33%
• Flow Measurement 33%

Engineering

• Particle Image Velocimetry 100%
• Energy Efficiency 50%
• Energy Conservation 50%
• Rod 50%
• Average Power 50%
• Leading Edge Vortex 50%
• Flow Measurement 50%
• Relative Location 50%
• Force Generation 50%
• Optical Filter 50%
• Oil Droplet 50%
• Deformation Characteristic 50%
• Relative Strength 50%
• Identical Dimension 50%
• Lift Force 50%
• Fixed Position 50%
• Aerodynamics 50%
• Flow Distribution 50%