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Please use this identifier to cite or link to this item: http://hdl.handle.net/2005/1477

Title: Helicopter Vibration Reduction Using Single Crystal And Soft Piezoceramic Shear Induced Active Blade Twist
Authors: Thakkar, Dipali
Advisors: Ganguli, Ranjan
Keywords: Helicopters - Vibration
Piezoceramics - Shear Dynamics
Rotors (Helicopters)
Helicopter Rotor Blades
Rotor Dynamics
Aeroelastic Analysis
Rotating Beams
Helicopters - Aerodynamics
Helicopter - Aeroelasticity
Rotar Blade
Piezoceramic Actuation
Helicopter Vibration Reduction
Helicopter Rotor
Submitted Date: Apr-2005
Series/Report no.: G19167
Abstract file URL: http://etd.ncsi.iisc.ernet.in/abstracts/1897/G19167-Abs.pdf
URI: http://hdl.handle.net/2005/1477
Appears in Collections:Aerospace Engineering (aero)

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