Objective
Flap systems are highly efficient lift providing elements in low speed flight. A potential measure to shift the stall onset to higher limits can be found in an Active Flow Control (AFC) approach by pulsed blowing. The majority of corresponding research aims at understanding the aerodynamic phenomenon allowing broad bandwidth investigations to find optimum configurations. In this proposal the systems aspects are addressed with respect to the active flow control actuator system. The overall system integration will be performed by the SFWA partner EADS-IW with support provided by TUB through this project.
Call for proposal
SP1-JTI-CS-2010-01
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Funding Scheme
JTI-CS - Joint Technology Initiatives - Clean SkyCoordinator
10623 Berlin
Germany