Stress concentration/intensity around elliptical/circular cylinder shaped surface flaws in cross-ply plates and validity of St. Venant’s principle in the presence of interacting singularities

Effects of localized elliptical (circular being a special case) cylindrical surface flaws in laminated composite plates are investigated by using C°-type triangular composite plate elements, formulated on the assumptions of transverse inextensibility and layer-wise constant shear-angle theory (LCST)...

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Vydáno v:	Applied mathematical modelling Ročník 37; číslo 3; s. 1362 - 1377
Hlavní autoři:	Chaudhuri, Reaz A., Sinan Oktem, A., Guedes Soares, C.
Médium:	Journal Article
Jazyk:	angličtina
Vydáno:	Elsevier Inc 01.02.2013
Témata:	Cross-ply laminate Elliptical or circular cylindrical surface hole Free-edge stress singularity Interaction of singularities St. Venant’s principle Stress concentration factor (SCF) Stress concentration factor (SCF) Free-edge stress singularity Interaction of singularities St. Venant’s principle Cross-ply laminate Elliptical or circular cylindrical surface hole
ISSN:	0307-904X
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Popis
Shrnutí:	Effects of localized elliptical (circular being a special case) cylindrical surface flaws in laminated composite plates are investigated by using C°-type triangular composite plate elements, formulated on the assumptions of transverse inextensibility and layer-wise constant shear-angle theory (LCST). Numerical results for a cross-ply laminate compromised by the presence of an external part-through elliptical/circular cylindrical slot indicate the existence of severe cross-sectional warping in the vicinity of the surface flaw and plate boundaries. Furthermore, three-dimensional nature of the stress concentration factor in the neighborhood of the elliptical or circular cylinder shaped surface flaw boundary is clearly exhibited. Besides, very high stress concentration factors are found in the layer weakened by the surface flaw. Most importantly, the effects of stress singularity in the neighborhood of the circumferential re-entrant corner lines of the elliptical/circular cylindrical surface flaws, weakening laminated composite plates, are numerically assessed, because of their role in crack initiation. Finally, the interaction of this singularity with free edge stress singularity at the plate boundary, and the implication of such interactions (i.e., violation of St. Venant’s principle) in regards to testing of laminated composite specimens are thoroughly investigated.
ISSN:	0307-904X
DOI:	10.1016/j.apm.2012.04.001