Design and Development of Piezoelectric Stack Actuated Trailing Edge Flap for Helicopter Vibration Reduction

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...

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Bibliographic Details
Main Author: Mallick, Rajnish
Other Authors: Ganguli, Ranjan
Language:en_US
Published: 2018
Subjects:
Piezoelectric Stack Actuators
Helicopter Vibration Control
Trailing Edge Flaps (TEFs)
Helicopter Aeroelastic Analysis
Rotors (Helicopters)
Piezoelectric Actuator Hysteresis
Flaps (Airplanes)
Heicopte r- Aerodynamics
Aeroelastic Optimization
Helicopter Rotor Blades
Helicopter Vibrations
Helicopter Vibration Reduction
Helicopter Trailing Edge Flap
Piezoelectric Stack Actuator (PEA)
Aerospace Engineering
Online Access:http://etd.iisc.ernet.in/handle/2005/2990
http://etd.ncsi.iisc.ernet.in/abstracts/3853/G26734-Abs.pdf

Internet

http://etd.iisc.ernet.in/handle/2005/2990
http://etd.ncsi.iisc.ernet.in/abstracts/3853/G26734-Abs.pdf

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