Pomilio, Ottorino · New York, McGraw-Hill · leaf 38
. By applying the data from these curves to a wing of 5 ft. chord and 40 ft. span, supposing the normal speed to be 100 m.p.h. and the normal angle of flight 2°, the wing loading will be L = 7.5 X 200 = 1500 lb. and it will be in equilibrium if the center of gravity of theload falls at a distance… … 17.5 15.0 12.5 10.0 7.5 5.0 2.5 > / I - * ■> ^ *c > ^ v^ ■» ^ ■^ • / 1 ^ w ^ ^^s y^ ^s /^ ^s / ^^ -^Z ^k_ tL ^^ ^^ ^- / ^^^^ ^^ 7 ^ /^ -?/ / ^^ 7 y / / - ( \j / A- 2C. c 0.50 0.45 0.40 0.35 0.30 0.25 0.20 0.15 -3-2-10 1234567 69Degrees.Fig. 25. and it will be applied at 37 per cent, of the…
Airplanes
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