Design and Development of Piezoelectric Stack Actuated Trailing Edge Flap for Helicopter Vibration Reduction
This research investigates on-blade partial span active plain trailing edge flaps (TEFs)with an aim to alleviate the helicopter vibrations. Among all the available smart materials, piezoelectric stack actuator(PEA)has shown its strong candidature for full scale rotor systems. Although, PEAs are quit...
Main Author: | Mallick, Rajnish |
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Other Authors: | Ganguli, Ranjan |
Language: | en_US |
Published: |
2018
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Subjects: | |
Online Access: | http://etd.iisc.ernet.in/handle/2005/2990 http://etd.ncsi.iisc.ernet.in/abstracts/3853/G26734-Abs.pdf |
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