Modeling and analysis of helicopter vibrations during dynamic conditions

dc.contributor.guide	Swamy R P	en_US
dc.coverage.spatial	Mechanical engineering	en_US
dc.creator.researcher	Shashidhara T	en_US
dc.date.accessioned	2014-07-07T05:23:43Z
dc.date.available	2014-07-07T05:23:43Z
dc.date.awarded		en_US
dc.date.completed	24/12/2012	en_US
dc.date.issued	2014-07-07
dc.date.registered	25/08/2009	en_US
dc.description.abstract	With increasing demand for passenger transportation and demand for high speed and high performance helicopters for defense vibration control has become an important design objective of modern helicopters so careful analysis is necessary to determine and eliminate source of vibration Vibration levels in helicopters are very high when compared to fixed wing aircraft There are many sources of vibration further lightweight aircraft structures have many natural frequencies and mode shapes	en_US
dc.description.note		en_US
dc.format.accompanyingmaterial	CD	en_US
dc.format.dimensions	xiv, 117p.	en_US
dc.format.extent	8x12	en_US
dc.identifier.uri	http://hdl.handle.net/10603/20337
dc.language	English	en_US
dc.publisher.institution	Department of Mechanical Engineering	en_US
dc.publisher.place	Shankaraghatta	en_US
dc.publisher.university	Kuvempu University	en_US
dc.relation	70	en_US
dc.rights	university	en_US
dc.source.university	University	en_US
dc.subject.keyword	Helicopter vibrations- Modeling; Mechanical engineering	en_US
dc.title	Modeling and analysis of helicopter vibrations during dynamic conditions	en_US
dc.title.alternative		en_US
dc.type.degree	Ph.D.	en_US