Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 265
shows thestresses in the fuselage due to the loads assumed. For the nomenclatureof the members see Fig. 168. The column in Table XXV headed Sec-tion, refers to the types of sections shown in Fig. 169. Where no di-mension is shown in Fig. 169, it is indicated in the table. It should be noted that… … 246 Art. 164 Summary of Stresses in Fuselage
Airplanes
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