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Wind tunnel tests on airfoil boundary control using a backward opening slot (1929)

NASA Technical Reports Server (NTRS) · leaf 14

An illustration from Wind tunnel tests on airfoil boundary control using a backward opening slot, 1929, leaf 14 — Fig.9. N.A.O.A. Technical Note No.323 30° 6° 13° 18° 34° 0° -60 Angle of attack, degrees Fig.9

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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