Abstract
This paper documents the development of Synthetic Jet Actuator (SJA) array hardware to augment high lift system effectiveness in a wind tunnel model. The work involved the design, manufacture and bench test of a SJA array based on an inclined actuator configuration to reduce volume installation requirements without a loss in jet velocity relative to a non-inclined baseline model; incorporation of proper SJA systems wiring and internal SJA chamber pressure-sensing for actuator health monitoring. The peak velocity obtained from the inclined SJA array was 100 m/s, which compares favorably to the baseline array (~90 m/s) while reducing usable depth requirements by 50 percent. The final outcome of this work has been to apply the design lessons learned to develop a methodology for designing a SJA array with the constraints of using piezoelectric-based actuator technology for flow separation control applications.
Original language | Undefined |
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Title of host publication | 6th AIAA Flow Control Conference 2012 |
Publication status | Published - 2012 |
Event | 6th AIAA Flow Control Conference 2012 - New Orelans, United States Duration: 25 Jun 2012 → 28 Jun 2012 Conference number: 98167 |
Conference
Conference | 6th AIAA Flow Control Conference 2012 |
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Country/Territory | United States |
City | New Orelans |
Period | 25/06/12 → 28/06/12 |