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

dc.contributor.advisor	Ganguli, Ranjan
dc.contributor.author	Thakkar, Dipali
dc.date.accessioned	2011-10-14T05:22:16Z
dc.date.accessioned	2018-07-31T05:14:48Z
dc.date.available	2011-10-14T05:22:16Z
dc.date.available	2018-07-31T05:14:48Z
dc.date.issued	2011-10-14
dc.date.submitted	2005
dc.identifier.uri	https://etd.iisc.ac.in/handle/2005/1477
dc.identifier.abstract	http://etd.iisc.ac.in/static/etd/abstracts/1897/G19167-Abs.pdf	en_US
dc.language.iso	en_US	en_US
dc.relation.ispartofseries	G19167	en_US
dc.subject	Helicopters - Vibration	en_US
dc.subject	Piezoceramics - Shear Dynamics	en_US
dc.subject	Rotors (Helicopters)	en_US
dc.subject	Helicopter Rotor Blades	en_US
dc.subject	Rotor Dynamics	en_US
dc.subject	Aeroelastic Analysis	en_US
dc.subject	Rotating Beams	en_US
dc.subject	Helicopters - Aerodynamics	en_US
dc.subject	Helicopter - Aeroelasticity	en_US
dc.subject	Rotar Blade	en_US
dc.subject	Piezoceramic Actuation	en_US
dc.subject	Helicopter Vibration Reduction	en_US
dc.subject	Helicopter Rotor	en_US
dc.subject.classification	Aeronautics	en_US
dc.title	Helicopter Vibration Reduction Using Single Crystal And Soft Piezoceramic Shear Induced Active Blade Twist	en_US
dc.type	Thesis	en_US
dc.degree.name	PhD	en_US
dc.degree.level	Doctoral	en_US
dc.degree.discipline	Faculty of Engineering	en_US

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