Wind Tunnel Testing of Passive High-Lift Systems

This paper presents experimental results obtained with passive high liftsystems 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 e...

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Bibliographic Details
Published in:INCAS bulletin 2012-01, Vol.4 (1), p.67-75
Main Authors: Pricop, Mihai Victor, Stoica, Corneliu, Nae, Catalin, Munteanu, Florin, Rosenblum, Jean-Pierre, Bobonea, Andreea, Brinza, Ionut
Format: Article
Language:English
Subjects:
Flaps
high lift system
smart kinematics flap
vortex generato
wind tunnel
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Summary:This paper presents experimental results obtained with passive high liftsystems 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. [PUBLICATION ABSTRACT]
ISSN:2066-8201
2247-4528
DOI:10.13111/2066-8201.2012.4.1.8