Pomilio, Ottorino · New York, McGraw-Hill · leaf 366
gures for components Rr and Ri,the former having been plotted in Fig. 217 and the latterin Fig. 218. The shearing stresses Rr and Rt being known, by meansof a new integration, the diagrams of the bending momentsMr and M« can easily be obtained. It should be notedthat the maximum value of Mr equals… … 352 AIRPL.WE DESiaX AND CONSTRUCTION therefore Mr = I X 10,500 11). X inch = 5280 lb. X mch.The scale of moments is fixed in this manner and conse-quently that of the shearing stresses; and thus the value ofthe coefficient A is also determined. Then, for each section,the resultant stress due to the…
Airplanes
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