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Uploaded by Holmes540 on Nov 11, 2010
NACA 0015 Airfoil test in wind tunnel at 20 m/s. Angle of Attack 0 to 15 degrees. Stall at ~12 degrees, flow reattachment at 10 degrees.Twitter: @Holmes540
Science & Technology
Standard YouTube License
wheres the smoke
hip50centboy 9 months ago
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wheres the smoke
hip50centboy 9 months ago