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

NASA Technical Reports Server (NTRS) · leaf 13

An illustration from Wind tunnel tests on airfoil boundary control using a backward opening slot, 1929, leaf 13
Dynamic pressure ««a-n.» 'lg.8 Increase in the ratio ,n cfr \ ^ . * . ,„ DS^ e 3 various Widths and pressures,

NASA Technical Reports Server (NTRS)

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

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