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Good Luck.
Not seeing anything in Suction and Blowing Flow Control on Airfoil for Drag
Reduction in Subsonic Flow that relates to brake cooling or inlet location.
I understand porous wings and imagine where the vents they don't show might be.*
What size ducting do you contemplate?
* Oops, there it is: The experiment examined both methods at the position of 25% of the chord-length of the airfoil at Reynolds number 1.2 x 10^5.
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