N.A.CA. Technical Memorandum No.578 Figs.7a,7b,8,9a,9b,10,11 Pig. 8 1.2 Ratios of 1.0 induced j\t0=6.5 m drag,tend- 0.8 ing and torsional 0.6 b -40 m moment.wing 0.4 chord and thickness in0.2 in the middle „ for the two w.ngs Figg>7a and ?b# Fig.7b a'Wi/wi min 1-081 C,T0/T0 '=1.141 b,M0/M0«.… … induced dragpwith b = 40 m(l31 ft.) a, P= -0.25 and F=220 m (23 58 sq.ft.) b, 0 = 0. c, p =+0.25 Fig.10 Drags and bending moments of circulation distributions in Fig.4 in comparison with the drags and bending moments of elliptical 120 distribution. 80 40 3a o -10 -8 -6 -4 -2 0 2 4 6 8 10 Fig.11 ca…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
