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Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch (1932)
NASA Technical Reports Server (NTRS) · leaf 8
145 EFFECT OF TABIATION OF CHOED AND SPAN OF AILERONS ON HINGE MOMENTS … Ptfch angle. Pitch angle FiGUxs 25.—CJark T wlog section. Cr versos pitch angle for ono FiGU&£ 27.--GIaric Y wing section. Combined Cr twsds pitch angle aUieroD. Aileron spen 20 fnclies. AOeroa chord 2.0 inches. Boll for one aOeron. Aileron span 20 Inches. AJIenui chord %Si Inches. ancle 0*>.…NASA Technical Reports Server (NTRS)
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