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: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Micro-air-vehicle;Design;Flapping;Piezo-electric actuators |
| Subjects: | ENGINEERING > Structural Mechanics ENGINEERING > Mechanical Engineering |
| Division/Department: | Structures Division |
| Depositing User: | Ms Indrani V |
| Date Deposited: | 16 Jan 2009 |
| Last Modified: | 24 May 2010 09:40 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1119 |
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