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Experimental and Computational Investigation of Piezoelectric Actuator Hysteresis Phenomenon in Helicopter Vibration Control using Dual Trailing Edge Flaps

Viswamurthy, SR and Ganguli, R (2006) Experimental and Computational Investigation of Piezoelectric Actuator Hysteresis Phenomenon in Helicopter Vibration Control using Dual Trailing Edge Flaps. In: 32nd European Rotorcraft Forum, September 12-14 2006, Maastricht, Netherlands.

Full text not available from this repository.
Item Type: Conference Paper
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 07 Dec 2011 05:17
Last Modified: 07 Dec 2011 05:17
URI: http://eprints.iisc.ernet.in/id/eprint/42210

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