Effect of Aerodynamic Design on Glider Performance (1935)
NASA Technical Reports Server (NTRS) · leaf 14
N.A.C.A. Technical Ivlemorand-um ITo. 762 km/h lu3 40 , 60 80 100 1 20 140 S I I I L X ra/ s g/?=1S kg/m2 v. Z m/ s cw =0.01 a, A = 16 "b, A = 20 Fig-are 5.-Effect of aspect ratio. … 5 7 9 11 A 1* 15 17 19 Figure 7.-0t tiiruin values for tits long-distance glider. - 2 V X in ( ?^m- + est v2vrn - Av/ p/2 A v V*m A „ * .-"Jbest 2 ln Uv~ v-A7y
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