Design and Implementation of Flapping Wing Actuators for a Micro-Air-Vehicle

Shaik, Imran (2005) Design and Implementation of Flapping Wing Actuators for a Micro-Air-Vehicle. Technical Report. National Aerospace Laboratories, Bangalore, India.

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Abstract

The project aims to use the multi-functional peizo-electric materials as actuators to vibrate the wings of MAV. Modeling the peizo-electric materials in the design of a flapping wing is the primary issue. Finite element analysis is performed to demonstrate the flapping action of designed wing.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Micro-air-vehicle;Design;Flapping;Piezo-electric actuators
Subjects: ENGINEERING > Structural Mechanics
ENGINEERING > Mechanical Engineering
Depositing User: Users 10 not found.
Date Deposited: 16 Jan 2009
Last Modified: 24 May 2010 04:10
URI: http://nal-ir.nal.res.in/id/eprint/1119

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