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Wind tunnel tests of correction formula for wings of large span (1924)

NASA Technical Reports Server (NTRS) · leaf 13

An illustration from Wind tunnel tests of correction formula for wings of large span, 1924, leaf 13 — N.A.C.A: Technical Mernorandiiin No. 263- Fig. 4 ® b= 60 cm (23.62 in. + " 90 " (35,43 " " (47.24 " X " 120 " (59.05 " O " 150 e " 180 " (70.87 " … 160 200 _80 -40 00 40 80 120 Fig. 4 Angle of attack,a

NASA Technical Reports Server (NTRS)

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