Design and test of synthetic jet actuator for small UAVS

Design and test of synthetic jet actuator for small UAVS

In this project synthetic jet actuators based on piezoelectric ceramic unimorph are designed and fabricated. Tests are done in both quiescent and crossflow conditions, results show that actuator performance depends on orifice location and actuation frequency. Besides flow visualization demonstrates...

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Main Author: Du, Jiaxing.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Final Year Project
Language:English
Published: 2012
Subjects:
DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Online Access:http://hdl.handle.net/10356/50560
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-505602023-03-04T19:17:48Z Design and test of synthetic jet actuator for small UAVS Du, Jiaxing. School of Mechanical and Aerospace Engineering Lau Gih Keong Tang Hui DRNTU::Engineering::Aeronautical engineering::Aerodynamics In this project synthetic jet actuators based on piezoelectric ceramic unimorph are designed and fabricated. Tests are done in both quiescent and crossflow conditions, results show that actuator performance depends on orifice location and actuation frequency. Besides flow visualization demonstrates actuators’ capability to suppress flow separation on LS (1)-0421 wing model. This lays the foundation for its potential application on unmanned aerial vehicle. Bachelor of Engineering (Aerospace Engineering) 2012-06-28T03:10:13Z 2012-06-28T03:10:13Z 2012 2012 Final Year Project (FYP) http://hdl.handle.net/10356/50560 en Nanyang Technological University 60 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Aerodynamics
spellingShingle DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Du, Jiaxing.
Design and test of synthetic jet actuator for small UAVS
description In this project synthetic jet actuators based on piezoelectric ceramic unimorph are designed and fabricated. Tests are done in both quiescent and crossflow conditions, results show that actuator performance depends on orifice location and actuation frequency. Besides flow visualization demonstrates actuators’ capability to suppress flow separation on LS (1)-0421 wing model. This lays the foundation for its potential application on unmanned aerial vehicle.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Du, Jiaxing.
format Final Year Project
author Du, Jiaxing.
author_sort Du, Jiaxing.
title Design and test of synthetic jet actuator for small UAVS
title_short Design and test of synthetic jet actuator for small UAVS
title_full Design and test of synthetic jet actuator for small UAVS
title_fullStr Design and test of synthetic jet actuator for small UAVS
title_full_unstemmed Design and test of synthetic jet actuator for small UAVS
title_sort design and test of synthetic jet actuator for small uavs
publishDate 2012
url http://hdl.handle.net/10356/50560
_version_ 1759858337682292736

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