Pomilio, Ottorino · New York, McGraw-Hill · leaf 355
0 6000 KOOOIn.lbs. Scale of Moments ?IG. 207. 340 AIRPLANE DESIGN AND CONSTRUCTION because with a great transversal load the wheel wouldbreak. In Fig. 209 the sections of the various membershave been given, the results of the analysis having been CASE 4-. … FRONT eLevATION SIDE ELEVATION Scale o-F Leng+hs400 lbs. D1A6R^M OF ENDING 6EAR
Airplanes
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