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
141 EFFECT OF VAEIATION OF CHORD AND SPAN OF AILERONS ON HINGE MOMENTS … 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 varying aileron chord— i 204n<2i span (87 per cent of wfng semi^an). Fitch angle…
NASA Technical Reports Server (NTRS)
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