Minimum consumption of fuel in airplane for given number of miles is primary factor and not weight of engine; speed at minimum drag; reciprocal relations of aerodynamic values; influence of decreasing weight of fuel during flight; variation of long-distance-flight conditions with altitude; influence of decreasing load of fuel on altitude of flight. (Aircraft Engineer Sec.) (See also Aeronautics (A.S.M.E. Trans) vol. 50, no. 26, Sept. pp. 21-27, 5 figs)
The theory of long distance flight
Flight
Flight ; 21 , n 17
1929
6 pages
5 Figs.
Article (Journal)
English
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