Thermoelastic analysis of a laminated composite skew plate with a circular cutout subjected to linearly varying temperature across the thickness

摘要: The behaviour of a laminated composite skew plate with hole subjected to temperature as well combined and transverse pressure loading has been investigated. A finite element method which works on the basis three-dimensional theory elasticity is employed evaluate deflection, in-plane stresses interlaminar stresses. results obtained by varying angle diameter are discussed. It observed that magnitude deflection in case more when compared respective values pure thermal loading. magnitudes for be less at higher angles, because distance between opposite sides decreases increase causing stiffness plate. solutions structures considered present analysis will useful construction safe efficient like bridges swept wings aircraft structures. IPC Code: C08