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Please use this identifier to cite or link to this item: https://shodhratna.thapar.edu:8443/jspui/handle/tiet/517
Title: Hygrothermal degradation of the composite laminates from woven carbon/SC-15 epoxy resin and woven glass/SC-15 epoxy resin
Authors: Jana, R. N.
Bhunia, H.
Keywords: Absorption
Aerospace engineering
Carbon fiber reinforced plastics
Dimensional stability
Flexural testing
Textile finishing
Issue Date: 2008
Abstract: The degradation mechanism for hygrothermal aging of woven carbon-epoxy and woven glass-epoxy composite laminates was investigated in the micro-scale. Inter-laminar shear and cross laminar flexural tests were performed on notched and unnotched specimens to know the mechanical performance of the composite laminates. The Interlaminar Shear Stress (ISS) for both the composites was also evaluated and correlated with the number of hygrothermal cycles. Four-point bending and tensile or compression shear loading configurations were also used. The stress at the onset of delamination (Delamination Damage Tolerance, DDT) was identified from the load-deflection curve of the flexural specimens and correlated with the number of hygrothermal cycles. It was found that both the ISS and DDT decrease with the exposure time. Dimensional stability was almost unchanged throughout the aging process, although there was a very little moisture absorption (∼1.3%) in glass-epoxy and carbon-epoxy composite laminates. SEM photomicrographs of the delaminated surface show that failure occurs suddenly in a macroscopically brittle mode by crack initiation and propagation method. © 2008 Society of Plastics Engineers. © 2008 Elsevier B.V., All rights reserved.
URI: https://shodhratna.thapar.edu:8443/jspui/handle/tiet/517
ISSN: 02728397
Appears in Collections:CH Journal Articles

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