Summary
This project adresses the development of two-stage no-moving-parts fluidic actuator systems for use in active flow control applications. The work is based on the actuator technology created in the EC-funded Clean Sky projects DT-FA-AFC, FloCoSys, and robustAFC, but goes vastly beyond the scope of those projects, by broadening the view to include real-aircraft constraints and considerations from other-than-aerodynamics disciplines. The project will enable higher TRL experiments to thoroughly validate the concept of local active flow control by pulsed air blowing and will provide a flow control system, which fulfils real-aircraft integration requirements. Through detailed research, it will further the understanding of this flow control actuator concept. Finally, the proposed research, innovation, and development work on the two-stage fluidic actuators of this project will beneficially impact the industrialization of local active flow control by contributing substantially to making such a flow control actuators available on aircraft system level.
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More information & hyperlinks
| Web resources: | https://cordis.europa.eu/project/id/715796 |
| Start date: | 01-06-2016 |
| End date: | 31-05-2019 |
| Total budget - Public funding: | 388 750,00 Euro - 388 750,00 Euro |
Cordis data
Original description
This project adresses the development of two-stage no-moving-parts fluidic actuator systems for use in active flow control applications. The work is based on the actuator technology created in the EC-funded Clean Sky projects DT-FA-AFC, FloCoSys, and robustAFC, but goes vastly beyond the scope of those projects, by broadening the view to include real-aircraft constraints and considerations from other-than-aerodynamics disciplines. The project will enable higher TRL experiments to thoroughly validate the concept of local active flow control by pulsed air blowing and will provide a flow control system, which fulfils real-aircraft integration requirements. Through detailed research, it will further the understanding of this flow control actuator concept. Finally, the proposed research, innovation, and development work on the two-stage fluidic actuators of this project will beneficially impact the industrialization of local active flow control by contributing substantially to making such a flow control actuators available on aircraft system level.Status
CLOSEDCall topic
JTI-CS2-2015-CFP02-LPA-01-07Update Date
27-10-2022
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