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Tests of N.A.C.A. airfoils in the variable-density wind tunnel Series 230. (1936)

NASA Technical Reports Server (NTRS) · leaf 13

An illustration from Tests of N.A.C.A. airfoils in the variable-density wind tunnel Series 230., 1936, leaf 13 — * 6 10 14 18 22 Maximum thickness in percent of chord figure 7.- Variation of lift and'drag characteristics with thickness ratio.

NASA Technical Reports Server (NTRS)

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

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