Inside Out Library · Explore
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 ,OfS ,030 .025 ,OfO .020 .0O5 Cm Cs 0 .010 -,005 JQOS 10* 29" 30^ or 40' W 20* 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… … P/fch angle Pitch angle PiGxmx 26.—Clark Y wfn^ section. Cs versus pitch angle ftir one FDGtTuc 28.—Clark Y wing section. Combhied Cm versos pitch angle aileron. Aileron span 20 Inches. Aileron chord 3.0 inches. Soli Cor one aileron. Afteron span 20 Inches. Aileron chord 3.0 Inches. Bon angle 0".…NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch
More like this
