EXPERIMENTAL OIL FLOW IMAGES
2nd
AIAA CFD High Lift Prediction Workshop
The following surface oil flow images are for the low-Reynolds number condition
(ReMAC=1.35 million), from the B-LSWT (Airbus
Low Speed Wind Tunnel in Bremen). These are all views looking down onto the wing upper surface.
AoA=7 deg:
AoA=18.5 deg:
AoA=21 deg:
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Last Updated: 10/26/2012