New wing and bumper look pretty awesome together. Some really useful testing done at Bedford last week. As expected, the central section of the wing is stalled at maximum AoA due to the air flow in this area being influenced by the rear window, increasing the AoA locally. You can see from pic 2 of the tuft tests that the outboard flow is still attached but the central section is stalled. At lower AoA settings the flow on the full wing is attached.
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