Record Details

Helicopter Vibration Reduction Using Single Crystal And Soft Piezoceramic Shear Induced Active Blade Twist

Electronic Theses of Indian Institute of Science

View Archive Info
 
 
Field Value
 
Title Helicopter Vibration Reduction Using Single Crystal And Soft Piezoceramic Shear Induced Active Blade Twist
 
Creator Thakkar, Dipali
 
Subject 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
Aeronautics
 
Contributor Ganguli, Ranjan
 
Date 2011-10-14T05:22:16Z
2011-10-14T05:22:16Z
2011-10-14
2005-04
 
Type Thesis
 
Identifier http://etd.iisc.ernet.in/handle/2005/1477
http://etd.ncsi.iisc.ernet.in/abstracts/1897/G19167-Abs.pdf
 
Language en_US
 
Relation G19167