A study of airplane ranges and useful loads (1920)
NASA Technical Reports Server (NTRS) · leaf 20
theory to any specific case now reduces _to the.greatest simplicity as follows: . Data required. Wf = weight fully loaded with fuel We=weight empty of fuel. it = angle of incidence for minimum .total resistance. .... 1, Calculate the maximum range for an all fuel load by equation 17 s-?(l5Ts)n and… … Objective. DistoiKt Fig. 8. Any ordinate such as. CD will give the maximum pounds of load that can be carried for an objective at distance OC. The distance DE will give the corresponding weight of gasolme to be carried. (See Fig. 6.) For usual machines (22)
NASA Technical Reports Server (NTRS)
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