Resume and analysis of NACA lateral control research (1937)
NASA Technical Reports Server (NTRS) · leaf 21
orting throughout the speed range, while the rolling moments no lift, the production of rolling moment by equal and and the stabilizing factors are greatly reduced at the opposite lift increments on the two wing halves will not lower speeds. result in a yawing moment because the lift increment… … <- Roof 1/ Reta five distance from wing center line Tip — (a) Rectangular. (b) 4:3 taper. .008 .006 = Art .004 ,0C^ 0 6 .8 Tip' 0 *Root <-Root Relative distance from wing center tine ' Tip-^Z (c) 2:1 taper. " "h"r,S"f r0,"nC >nKim — " r^h* the elhcte „, ,„,„ JirZion „ ail,™ wilh str,cbt w„ lapercu…
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