Wind Tunnel Testing of Passive High-Lift Systems

Wind Tunnel Testing of Passive High-Lift Systems

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...

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Bibliographic Details
Main Authors: Andreea BOBONEA, Florin MUNTEANU, Jean-Pierre ROSENBLUM, Catalin NAE, Corneliu STOICA, Mihai Victor PRICOP, Ionut BRINZA
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2012-03-01
Series:INCAS Bulletin
Subjects:
high lift system
wind tunnel
vortex generato
smart kinematics flap
Online Access:http://bulletin.incas.ro/files/pricop_stoica_nae_munteanu_rosenblum_bobonea_brinz.pdf
Description
Summary: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.
ISSN:2066-8201
2247-4528

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