Effects of thermal residual stresses on failure of co-cured lap joints with steel and carbon fiber-epoxy composite adherends under static and fatigue tensile loads

Cited 33 time in webofscience Cited 0 time in scopus
  • Hit : 362
  • Download : 0
A co-cured joint, which uses excess resin extracted from the composite material (or the polymer material) as the adhesive, has several advantages compared with the adhesively bonded joint. It has no need of the surface treatment of the composite adherend and any adhesive for bonding. In addition, its manufacturing process is very simple because the bonding process is achieved during the curing process of the composite adherend. Thermal residual stresses are important in analyzing failure of the co-cured joint because composite materials are different from metal alloys in thermal and mechanical properties. In general, effects of the thermal residual stresses on failure of the adhesive joint are analyzed through experimental and analytical results. Therefore in this paper, two design parameters, namely the surface roughness of the steel adherend and the stacking sequence of the composite adherend, are considered for static and fatigue tensile tests of the co-cured single and double lap joints. Stress distribution at the inter-face between the two adherends is used to analyze failure of the co-cured lap joints through the finite element method. Based on the stress distribution, two failure criteria, namely the three-dimensional Tsai-Wu failure criterion and the Ye-delamination failure criterion, are considered to predict the tensile load bearing capacity of the co-cured lap joints. Finally, effects of thermal residual stresses on failure of the co-cured single and double lap joints with the steel and composite adherends under static and fatigue tensile load conditions are presented through comparing the experimental and analytical results. (c) 2005 Elsevier Ltd. All rights reserved.
Publisher
ELSEVIER SCI LTD
Issue Date
2006
Language
English
Article Type
Article
Keywords

BEARING CAPACITY; BOND PARAMETERS; SINGLE; STRENGTH; DESIGN; MANUFACTURE; PREDICTION; ALUMINUM; SHAFTS

Citation

COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, v.37, no.3, pp.476 - 487

ISSN
1359-835X
DOI
10.1016/j.compositesa.2005.03.031
URI
http://hdl.handle.net/10203/92469
Appears in Collection
ME-Journal Papers(저널논문)
Files in This Item
There are no files associated with this item.
This item is cited by other documents in WoS
⊙ Detail Information in WoSⓡ Click to see webofscience_button
⊙ Cited 33 items in WoS Click to see citing articles in records_button

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0