Inside Out Library · Explore
Wind Tunnel Tests on an Airfoil Equipped with a Split Flap and a Slot (1929)
NASA Technical Reports Server (NTRS) · leaf 8
N.A.CA. Technical Note No. 324 Fig.3,4 … Fig.3 N.A.CA. 84 Airfoil with split flap-slot combination. ± .6 .a •Wit h slqt >4~ 1.4 .7 | -Wi t hout i slot b' , 1 0" /i 1.2 .6 - ■ 4" // Lift jcoeff icier ■+ 1.0 .5 -■- JL .8 .4 & y/f Drdg coefficient1 /' ; i y% D HP .6 .3 / i 4- .0' .4 .2 +,1 .2 .1 0 0 / -.2 ^ o 0; 8V 16 24 Angle of attack…NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Wind Tunnel Tests on an Airfoil Equipped with a Split Flap and a Slot
More like this
