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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 10

An illustration from Tests of N.A.C.A. airfoils in the variable-density wind tunnel Series 230., 1936, leaf 10 — .2 A .6 .8 1.0 1.2 /.4 1.6 1.8 -4 -2 0 -8 -4 0 4 8 12 16 20 24 28 32 Angle of attack, a (degrees) Lift coefficient, cl( Fijure A.- KAjC.A. £3015 airfoil

NASA Technical Reports Server (NTRS)

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

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