Wind tunnel AVERT model
Journal Title: INCAS BULLETIN - Year 2009, Vol 1, Issue 1
Abstract
The AVERT project aims to asses the oscillatory blowing on the flap for a high-lift configuration (wing with flap), and involves both experimental (low speed wind tunnel INCAS) and numerical activities. At low speed the active flow control may lead to a reduction or elimination of the flow separation on the high-lift devices, such as flaps, and involves the introduction or re distribution of momentum within the boundary layer. High-lift systems utilized as particular profiles at a certain offset of the main wing may solve the disagreement between the requirements of cruise flight and landing, especially for low velocity take-off.
Authors and Affiliations
Adrian DOBRE
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- EP ID EP160540
- DOI 10.13111/2066-8201.2009.1.1.19
- Views 92
- Downloads 0
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