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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
523 AIRFOILS HAVING THE MAXIMUM CAMBER UNUSUALLY EAR FORWARD … •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 tunnel-wall effect Corrected to infinite aspect ratio , 1.4 16 IB .2 .4 .6 .8…NASA Technical Reports Server (NTRS)
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