Wind Tunnel Testing of Passive High-Lift Systems
Journal Title: INCAS BULLETIN - Year 2012, Vol 4, Issue 1
Abstract
This paper presents experimental results obtained with passive high lift systems using a combination of smart flap kinematics and vortex generators. A mid-scale 2.5D wind tunnel model based on DLR-F15 is tested in INCAS Subsonic Wind Tunnel, swept at 30 deg, incorporating the slat, 54 flap/VG/chord extension configurations and test matrix, developed by Dassault-Aviation. INCAS designed, manufactured and instrumented components to be added to the existing INCAS-F15 2D wind tunnel model. The test campaign was completed and results are presented.
Authors and Affiliations
Mihai Victor PRICOP, Corneliu STOICA, Catalin NAE, Florin MUNTEANU, Jean-Pierre ROSENBLUM, Andreea BOBONEA, Ionut BRINZA
Keywords
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- EP ID EP150729
- DOI 10.13111/2066-8201.2012.4.1.8
- Views 109
- Downloads 0
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