Design, modeling, and testing of a fluidic flexible matrix composite damped absorber prototype for stiff-inplane hingeless rotorcraft blades

Keyphrases

• Absorber 100%
• Rotorcraft 100%
• Fluidic Flexible Matrix Composites 100%
• Rotor Blade 66%
• Low Weight 33%
• Rotor 33%
• Small Strain 33%
• Damper 33%
• Tip Displacement 33%
• Bending Strain 33%
• High Damping 33%
• Added Damping 33%
• Internal Water Pressure 33%
• Coaxial Configuration 33%
• Shaker Excitation 33%

Engineering

• Rotorcraft 100%
• Rotor Blade 100%
• Fluidics 100%
• Full Scale 50%
• Simulation Result 50%
• Rotors 50%
• Experimental Result 50%
• Fluid Pressure 50%
• Internal Fluid 50%
• Rotorcraft Structure 50%