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(Reference retrieved automatically from Web of Science through information on FAPESP grant and its corresponding number as mentioned in the publication by the authors.)

The relationship between pure delamination modes I and II on the crack growth rate process in cracked lap shear specimen (CLS) of 5 harness satin composites

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Author(s):
Shiino, M. Y. [1] ; Alderliesten, R. C. [2] ; Donadon, M. V. [3] ; Cioffi, M. O. H. [4]
Total Authors: 4
Affiliation:
[1] UNESP Univ Estadual Paulista, Inst Ciencia & Tecnol, Dept Engn Ambiental, BR-12247004 Sao Jose Dos Campos, SP - Brazil
[2] Delft Univ Technol TUDelft, Fac Aerosp Engn, Aerosp Struct & Mat, NL-2629 HS Delft - Netherlands
[3] ITA, BR-12228900 Sao Jose Dos Campos, SP - Brazil
[4] UNESP Univ Estadual Paulista, Fac Engn Guaratingueta, Dept Mat & Tecnol, Fatigue & Aeronaut Mat Res Grp, BR-12516410 Guaratingueta, SP - Brazil
Total Affiliations: 4
Document type: Journal article
Source: COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING; v. 78, p. 350-357, NOV 2015.
Web of Science Citations: 2
Abstract

Carbon fiber reinforced polymers (CFRP) structure can include dropping-off plies in order to comply with design requirements aiming at significant weight savings. However this type of discontinuity represents a potential source of delamination initiation and propagation which requires assessment of the mechanisms acting at the crack tip. This research investigates the influence of delamination modes I and II on the overall damage process observed in CLS specimen subjected to cyclic loads. The main contribution of this work focuses on the identification and physical interpretation of complex failure mechanisms in harness satin fabric. For this purpose a detailed fractographic analysis was carried out to qualitatively assess the surface fractures in these type of laminates. Results obtained for cyclic loaded CLS specimens were compared to analytical closed form solutions available in the literature. Results indicated that delamination front exhibited distinguishable delamination modes land II propagating at constant mixed mode ratio (G(I)/G(T)). (C) 2015 Elsevier Ltd. All rights reserved. (AU)

FAPESP's process: 11/01937-0 - Crack growth rate in 5HS carbon/epoxy composites manufactured by RTM: Relationship between axial loadings with pure modes of delamination I and II
Grantee:Marcos Yutaka Shiino
Support Opportunities: Scholarships in Brazil - Doctorate
FAPESP's process: 12/07646-0 - Evaluation of pressure gradient effect of RTM process on 5HS laminate by conducting DCB fatigue test
Grantee:Marcos Yutaka Shiino
Support Opportunities: Scholarships abroad - Research Internship - Doctorate