Instability of a cracked cylindrical shell reinforced by ...
2013-6-7 · Ateach shell cross section, the axes x, y and z are oriented along the longitudinal, tangential and radial direction of the cylinder, respectively, with their origin on the neutral surface. We consider an element cut out of the composite lamina by two pairs of planes parallel to the xz and yz planes as shown in Fig. 1(B). The bending
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