Resume and analysis of NACA lateral control research (1937)
NASA Technical Reports Server (NTRS) · leaf 21
d 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 Figure 12 gives a comparison of theoretical and vectors are all inclined backward by the induction, experimental… … (c) 2:1 taper. " "h"r,S"f r0,"nC >nKim — " r^h* the elhcte „, ,„,„ JirZion „ ail,™ wilh str,cbt w„ lapercu wim^n.
NASA Technical Reports Server (NTRS)
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