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Residual Stress Assessment in Thin Angle Ply Tubes
Authors:A. S. Kaddour  S. T. S. Al-Hassani  M. J. Hinton
Affiliation:(1) Future Systems Technology, A7 Building, QinetiQ, Ively Rd, Farnborough, Hampshire, GU14 0LX, UK;(2) Mechanical, Aerospace and Manufacturing Engineering Department, UMIST, P.O. Box 88, Manchester, M60 1QD, UK;(3) Future Systems Technology, QinetiQ, Fort Halstead, Sevenoaks, Kent, TN14 7BP, UK
Abstract:This preliminary study aims to investigate the residual stresses developed in hot cured thin-walled angle-ply filament wound tubes made of E-glass/epoxy, Kevlar/epoxy and carbon/epoxy materials. The residual stresses were estimated from change in geometry of these tubes when axially slitted at ambient temperature. Three basic deformation modes; namely opening up, closing-in and twisting, were observed and these depended on the winding angle, material and wall thickness. The residual stresses were also determined from hoop and axial strain gauges mounted on both the inner and outer surfaces at various locations around the tube. The stresses were compared with theoretical prediction based upon a linear thermo-elastic analysis. Both the predicted and measured values were found to increase with increasing hoop stiffness but there was a large discrepancy between the predicted and measured data, reaching a factor of 5 for the thinnest case. When compared with predicted failure stresses, the experimentally determined stresses were some 15% of the computed compressive strength.
Keywords:angle ply  kevlar  carbon  glass composite rings  slitting  residual thermal stress release  twisting
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