Inside Out Library · Explore

The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel (1932)

NASA Technical Reports Server (NTRS) · leaf 6

An illustration from The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel, 1932, leaf 6
551 TBDB AERODTlfAMIC CHABACTBEISTICS OF AIKFOILS … Angle ofoffack in degrees, a Lift caefffctenf (Absa/ufe), TIOUBX 8.—K. A. C. A. 8321 alrtoll. .09 ^-07 28' O •J ^.06 Z4' •l05 20' Q.04 /6° O ^M3 12 XI/ o -a* 1% -.4 .2 .4 .6 .a £0 • L2 4 8 /2 16 20 iCz/jf coefficieni (Absatuie), Cc Angle of atfactf in degrees, cL FiouBK B.—K. A. C. A. 103 abfolL…

NASA Technical Reports Server (NTRS)

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

More pictures from The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel

More like this