 ... independently, and to compute their separate effects, add the resulting stresses together, and to dimension the member accordingly. In the following analysis they are treated as acting simultaneously and the true cross-bending stresses found.  The Principles of Structural Design - الصفحة 180بواسطة George Kenneth Scott-Moncrieff - 1897عرض كامل - لمحة عن هذا الكتاب
 | John Butler Johnson, Charles Walter Bryan, Frederick Eugene Turneaure - 1903 - عدد الصفحات: 668
...cross-bending stresses found. 142. Derivation of a General Formula for Combined Stresses. Let M^ = bending moment at point of maximum deflection, from...deflection of member from all causes acting simultaneously • M, = bending moment from the direct loading, P, into its arm, v, , — Pv. ; P = total direct loading... | |
 | John Butler Johnson, Charles Walter Bryan, Frederick Eugene Turneaure - 1904 - عدد الصفحات: 698
...cross-bending stresses found. 142. Derivation of a General Formula for Combined Stresses. Lst M. = bending moment at point of maximum deflection, from...deflection of member from all causes acting simultaneously; Mt = bending moment from the direct loading, P, into its arm, •vl , = Pv. ; P = total direct loading... | |
 | John Butler Johnson, C. W. Bryan, Frederick Eugene Turneaure - 1904 - عدد الصفحات: 696
...cross bending stresses found. 142. Derivation of a General Formula for Combined Stresses. Let M, = bending moment at point of maximum deflection, from...from eccentricity of position of longitudinal loading ; •v, — maximum deflection of member from all causes acting simultaneously Mt = bending moment... | |
 | 1905 - عدد الصفحات: 912
...tension. The method of calculating by the third method is given by the following formula, in which M, = bending moment at point of maximum deflection, from...eccentricity of position of longitudinal loading; d = maximum deflection of member from all causes acting simultaneously; W, = total direct loading on... | |
 | 1905 - عدد الصفحات: 966
...tension. The method of calculating by the third method is given by the following formula, in which Mt = bending moment at point of maximum deflection, from...eccentricity of position of longitudinal loading; d = maximum deflection of member from all causes acting simultaneously; Wi = total direct loading on... | |
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