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

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dc.contributor.authorViswamurthy, S.R.
dc.contributor.authorGanguli, R.
dc.date.accessioned2016-07-01T14:38:13Z
dc.date.available2016-07-01T14:38:13Z
dc.date.issued2006
dc.identifier.otherAR05
dc.identifier.urihttp://hdl.handle.net/20.500.11881/1084
dc.language.isoen
dc.titleExperimental and computational investigation of piezoceramic actuators hysteresis phenomenon in helicopter vibration control using dual trailing-edge flaps

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