Pomilio, Ottorino · New York, McGraw-Hill · leaf 403
388 AIRPLANE DESIGN AND CONSTRUCTION the point of .support of the tail skid into two parts Xi andX2 so that xi ^ W_ __ X2 W + W … Fio. 24G. for which Xx V/ xi + X2 W + W + W SAND TESTS—WEIGHING—FLIGHT TESTS 389
Airplanes
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