A theory for primary failure of straight centrally loaded columns (1938)
NASA Technical Reports Server (NTRS) · leaf 2
the axis of rotation and when buckling must be no restraint of longitudinal displacements at occurs, there must be complete restraint of longitudinal displacements at the ends of the column. Because the ends of the column. When primary failure occurs in the manner shown in figure 3 (b), the twist… … Figure 3.—End conditions for different effective lengths, £0. , QJ, Cbt t'E the result that longitudinal bending stresses are present column, £0=9- for this case. Similarly, for any degree in addition to the shearing stresses of twisting. The end of restraint against longitudinal displacements of…
NASA Technical Reports Server (NTRS)
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