f the c values is not surprising when it is considered that the strength of the elevator and stabilizer was found according to other than the above-mentioned principles. From this tabulation the following general conclusions can be dra^vn: (a) Airplanes of similar construction, coming from the same… … Toto/ weighf-G-kg. _ n q ?200 Fig. 32.—Factor c in relation to total weight G. Cr This formula holds good for airplane weights between 800 and 5,000 kg. It is plotted in Figure 32 and shows that most experimentally obtained c values are lower than those calcu- lated from the rule. The value c = 2,…
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