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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| Format: | Final Year Project (FYP) |
| Language: | English |
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2012
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| Online Access: | http://hdl.handle.net/10356/50560 |
| _version_ | 1824456767460868096 |
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| author | Du, Jiaxing. |
| author2 | School of Mechanical and Aerospace Engineering |
| author_facet | School of Mechanical and Aerospace Engineering Du, Jiaxing. |
| author_sort | Du, Jiaxing. |
| collection | NTU |
| 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. |
| first_indexed | 2025-02-19T03:59:20Z |
| format | Final Year Project (FYP) |
| id | ntu-10356/50560 |
| institution | Nanyang Technological University |
| language | English |
| last_indexed | 2025-02-19T03:59:20Z |
| publishDate | 2012 |
| record_format | dspace |
| spelling | ntu-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 |
| spellingShingle | DRNTU::Engineering::Aeronautical engineering::Aerodynamics Du, Jiaxing. Design and test of synthetic jet actuator for small UAVS |
| title | 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_short | Design and test of synthetic jet actuator for small UAVS |
| title_sort | design and test of synthetic jet actuator for small uavs |
| topic | DRNTU::Engineering::Aeronautical engineering::Aerodynamics |
| url | http://hdl.handle.net/10356/50560 |
| work_keys_str_mv | AT dujiaxing designandtestofsyntheticjetactuatorforsmalluavs |