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Tests in the variable-density wind tunnel of related airfoils having the maximum camber unusually far forward (1936)
NASA Technical Reports Server (NTRS) · leaf 2
4 40 321 28$ .d" v. 20 o /eg ■8 r-5 i ■§ a Airfoil: MA.Cjf. 21012 R.H:3,200,000 •6 Size: 5-X.30' Vel.(ff./sec): 68.4 -12 ■-.2 -4 Airfoil: MACA. 2/0/2 R.N.:3,200,000 Pres.(st'nd.oim):2I.O Dote:4-24-34 Where tested: LMA.L. Test: V.D.T. 1126 Date: 4-24-34 Test: V. D.T. 1126 o -16 -.4 \-4 Corrected for… … Airfoil: N.A.C^. 22012 R.N.:3,170,000 o X Size: 5x30" Vei.ftt./sec): 69.1 __? -12 -.3 Pres.(sthd.atm):20£ Date: 4-23-34 ■ Where tested: LM.A.L. Test:V.D.T.II25 o -18 -.4 ■8 Corrected for tunnel-wall effect. .2 .4 .6 .8 1.0 1.2 1.4 1.6 1.8 -.4 -.2 28 32 -8 -4 0 4 8 12 16 20 24 Angle of attack, ct…NASA Technical Reports Server (NTRS)
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