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

NASA Technical Reports Server (NTRS) · leaf 9

An illustration from Wind tunnel tests on airfoil boundary control using a backward opening slot, 1929, leaf 9 — Wing pressure Dynamic pressure Fig,4 Increase in maximum lift due to slot at various widths and wing pressure.

NASA Technical Reports Server (NTRS)

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

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