Pomilio, Ottorino · New York, McGraw-Hill · leaf 53
oefficient of penetration of the fuselage. Thelower K is, the more suitable will be the fuselage, as thecorresponding necessary power will be decreased. Equation (1) shows two ways of decreasing the necessarypower; (a) By reducing the major section of the fuselage to a minimum, and (6) by lowering… … Fr;. 38. fuselage may be of circular, square, rectangular, triangular,etc., section, so designed that its major section follows theform of the major section of the engine. Inthe second place, it is good practice, when otherreasons do not prevent it, to arrange the variousmasses constituting the…
Airplanes
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