Tests in the variable-density wind tunnel of related airfoils having the maximum camber unusually far forward (1936)
NASA Technical Reports Server (NTRS) · leaf 5
526 REPORT NATIONAL ADVISORY COMMITTEE FOR AEBONATJTICS … Lift coefficient, & Angle of attack, a (degrees) FlGUBE 8.—N. A. O. A. 23112 airfoIL .12. .11 .10 .09 .44 los .40 o .s •s 07 .36 s. o t> t> 06 .32 o c u <n 28~Z 05 .28 11 0 24H i. .04 ■<3- 20 s |- .03 .u /6£ . ■ 02 cj o ,2% 12 0/ ■2 u 5^/00 .08 0 4% .2 .04 o -./ o .o 4 -.2 -.3 Airfoil:N.A.C.A.…
NASA Technical Reports Server (NTRS)
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