Experimental and computational investigation of piezoceramic actuators hysteresis phenomenon in helicopter vibration control using dual trailing-edge flaps

dc.contributor.author	Viswamurthy, S.R.
dc.contributor.author	Ganguli, R.
dc.date.accessioned	2016-07-01T14:38:13Z
dc.date.available	2016-07-01T14:38:13Z
dc.date.issued	2006
dc.identifier.other	AR05
dc.identifier.uri	http://hdl.handle.net/20.500.11881/1084
dc.language.iso	en
dc.title	Experimental and computational investigation of piezoceramic actuators hysteresis phenomenon in helicopter vibration control using dual trailing-edge flaps

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