Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch (1932)
NASA Technical Reports Server (NTRS) · leaf 4
.015 ,oto MfO ,005 .005 o Cj, O -.005 -,005 .o/o ■^.OlO -.0/5 -M/5 -.020 -.oeo 15 20 25 30 35 \ 15 20 25 30 ^5 Per cent aileron chord of wing chord i Per cent aileron cfrord of wing chord FiGCBE 0.—Ciarfe Y wing section. Cn for varying aOeron chord—20- I FiouBB XL—U. d. A. 37 wfng sectfon. Ca fbr… … 33}^ , 50 ^ ^ se% Per cent aileron span of wing ssmfspan Percent aiferon span of wing semi span FiOUEE 10.—Clark Y ?rlng section. Cm for vaijing ^an—2^fnch FiGURi 12.—tJ. S. A. 27 wing section. Cm foe varying aOeron spnn— chord (25 per cent of wing chord)» FItdi angle VP. Ron angle 0". Scinch chord…
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