Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 32
ly to thetotal moment or shear at any point, but to the moment or shear causedby any individual load. The complete computations for the reactions, shears, and bendingmoments for a beam loaded as shown in Fig. 15 are as follows: 12 Art. 17 Calculation of Moments and Shears CALCULATION OF… … -4375 Fig. 17. Moment Diagram13 Strength of Materials Art. 17 G enM/nn-^ rer>3/on- Posmi/e Momenf J-A7
Airplanes
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