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Pressure Distribution Over a Symmetrical Airfoil Section with Trailing Edge Flap (1931)

NASA Technical Reports Server (NTRS) · leaf 7

An illustration from Pressure Distribution Over a Symmetrical Airfoil Section with Trailing Edge Flap, 1931, leaf 7 — REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Figure 5

NASA Technical Reports Server (NTRS)

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

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