Pomilio, Ottorino · New York, McGraw-Hill · leaf 231
W/. // x ^ ^ v/^ ^ y^ ^ r.o 1.2 1.3 1.4 1.5 1.& 1.7 1.8 1.9 2.0Wf reduce the specific consumption to half, the radius of actionwould be doubled. 3. Upon the ratio between the total weight of the airplaneand this weight diminished by the quantity of gasohne and 216 AIRPLANE DESIGN AND… … .1 1.2 1.3 1.4 15 1.6 1.7 l.a 1.9 2.0 Fm. 140. We see, consequently, that the essential difference betweenthe formula of the useful load and that of the cruising radiusis in the fact that in the latter the total specific con-sumption of the engine, an element which did not even ORE AT LOADS AND…
Airplanes
Internet Archive · Public Domain Mark 1.0. Free to use for anything.
