Hygrothermal effects on quasi-isotropic carbon epoxy laminates with machined and molded edges
被引:30
作者:
Candido, G. M.
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Inst Aeronaut, Div Mat, BR-12228904 Sao Jose Dos Campos, SP, Brazil
Espacol Ctr Tecn Aerospacial, BR-12228904 Sao Jose Dos Campos, SP, BrazilInst Technol Aeronaut, Dept Engn Aeronaut & Mecan, BR-12228900 Sao Jose Dos Campos, SP, Brazil
Candido, G. M.
[2
,3
]
Costa, M. L.
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机构:
Inst Aeronaut, Div Mat, BR-12228904 Sao Jose Dos Campos, SP, Brazil
Espacol Ctr Tecn Aerospacial, BR-12228904 Sao Jose Dos Campos, SP, BrazilInst Technol Aeronaut, Dept Engn Aeronaut & Mecan, BR-12228900 Sao Jose Dos Campos, SP, Brazil
Costa, M. L.
[2
,3
]
Rezende, M. C.
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机构:
Inst Aeronaut, Div Mat, BR-12228904 Sao Jose Dos Campos, SP, Brazil
Espacol Ctr Tecn Aerospacial, BR-12228904 Sao Jose Dos Campos, SP, BrazilInst Technol Aeronaut, Dept Engn Aeronaut & Mecan, BR-12228900 Sao Jose Dos Campos, SP, Brazil
Rezende, M. C.
[2
,3
]
Almeida, S. F. M.
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Inst Technol Aeronaut, Dept Engn Aeronaut & Mecan, BR-12228900 Sao Jose Dos Campos, SP, BrazilInst Technol Aeronaut, Dept Engn Aeronaut & Mecan, BR-12228900 Sao Jose Dos Campos, SP, Brazil
Almeida, S. F. M.
[1
]
机构:
[1] Inst Technol Aeronaut, Dept Engn Aeronaut & Mecan, BR-12228900 Sao Jose Dos Campos, SP, Brazil
[2] Inst Aeronaut, Div Mat, BR-12228904 Sao Jose Dos Campos, SP, Brazil
[3] Espacol Ctr Tecn Aerospacial, BR-12228904 Sao Jose Dos Campos, SP, Brazil
Polymer matrix composites, when exposed to temperature and humid environment, undergo dimensional and stress state changes due to moisture induced swelling and thermal expansion. Moisture absorption may induce mechanical and physic-chemical changes that toughen the polymeric matrix and/or deteriorate matrix-fiber interface by interface debonding or micro-cracking. In the present paper, the effect of edge finishing combined with hygrothermal conditioning on the tensile strength of quasi-isotropic laminates is experimentally investigated. The results indicate that moisture may either increase or decrease the tensile strength of quasi-isotropic laminates with machined or molded edges depending on dominant effect (matrix toughening vs interface degradation). Transverse sections of specimens were observed by scanning electronic microscopy (SEM). (C) 2007 Elsevier Ltd. All rights reserved.
机构:
EMPRESA BRASILEIRA AERONAUT,DIV COMPOSITE MAT,BR-12225 S JOSE CAMPO,BRAZILEMPRESA BRASILEIRA AERONAUT,DIV COMPOSITE MAT,BR-12225 S JOSE CAMPO,BRAZIL
DEALMEIDA, SFM
CANDIDO, GM
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机构:
EMPRESA BRASILEIRA AERONAUT,DIV COMPOSITE MAT,BR-12225 S JOSE CAMPO,BRAZILEMPRESA BRASILEIRA AERONAUT,DIV COMPOSITE MAT,BR-12225 S JOSE CAMPO,BRAZIL
机构:
EMPRESA BRASILEIRA AERONAUT,DIV COMPOSITE MAT,BR-12225 S JOSE CAMPO,BRAZILEMPRESA BRASILEIRA AERONAUT,DIV COMPOSITE MAT,BR-12225 S JOSE CAMPO,BRAZIL
DEALMEIDA, SFM
CANDIDO, GM
论文数: 0引用数: 0
h-index: 0
机构:
EMPRESA BRASILEIRA AERONAUT,DIV COMPOSITE MAT,BR-12225 S JOSE CAMPO,BRAZILEMPRESA BRASILEIRA AERONAUT,DIV COMPOSITE MAT,BR-12225 S JOSE CAMPO,BRAZIL