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Advanced Composite Materials Volume 28, 2019 - Issue 4
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Articles

Analytical investigation of thermal and mechanical load effects on stress distribution in adhesive layer of double-lap metal-composite bonded joints

Hisashi KumazawaStructures and Advanced Composite Research Unit, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Tokyo, JapanCorrespondence[email protected]
&
Toshiyuki KasaharaStructures and Advanced Composite Research Unit, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Tokyo, Japan
Pages 425-444 | Received 08 Aug 2018, Accepted 24 Jan 2019, Published online: 10 Feb 2019

References

  • Volkersen O. Die niektraftverteilung in zugbeanspruchten mit konstanten laschenquerschritten. Luftfahrtforschung. 1938;15:4–41.
  • Goland M, Reissner E. The stresses in cemented joints. J Appl Mech. 1944;11:A17–A27.
  • Hart-Smith LJ. Adhesive-bonded double-lap joints. Washington (DC): NASA CR-112235; 1973.
  • Chen WT, Nelson CW. Thermal stress in bonded joints. IBM J Res Dev. 1979;23:179–188.
  • Tsai MY, Oplinger DW, Morton J. Improved theoretical solutions of adhesive joints. Int J Solids Struct. 1998;35:1163–1185.
  • Tsai MY, Morton J. An investigation into the stresses in double-lap adhesive joints with laminated composite adherends. Int J Solids Struct. 2010;47:3317–3325.
  • Ishii K, Imanaka M, Nakayama H, et al. Evaluation of the fatigue strength of adhesively bonded CFRP/metal single and single-step double-lap joints. Compos Sci Tech. 1999;59:1675–1683.
  • Yang C, Sun W, Tomblin JS, et al. A semi-analytical method for determining the strain energy release rate of cracks in adhesively-bonded single-lap composite joints. J Compos Mat. 2007;41:1579–1602.
  • Yang C, Chadegani A, Tomblin JS. Strain energy release rate determination of prescribed cracks in adhesively-bonded single-lap composite joints with thick bondlines. Compos Part B. 2008;39:863–873.
  • McCarville DA, Guzman JC, Weetin JL, et al. Manufacturing overview of a 2.4 meter (7.9 Foot) composite cryotank. SAMPE J. 2013;49:7–13.
  • Yoshimura A, Ogasawara T, Suemasu H. Validation of thermal stress reduction design of CFRP cryogenic propellant tank by LN2 immersion test. Tokyo, Japan: JAXA Research and Development Memorandum, JAXA-RM-12-012; 2013. (in Japanese).
  • Khoshravan M, Mehrabadi FA. Fracture analysis in adhesive composite material/aluminum joints under mode-I loading; experimental and numerical approaches. Int J Adhes Adhes. 2012;39:8–14.
  • Yokozeki T. Energy release rates of bi-material interface crack including residual thermal stresses: application of crack tip element method. Eng Fract Mech. 2010;77:84–93.
  • Technical datasheet of 3 M Scotch-Weld Structural Adhesive Film AF 163-2. 2009 Nov.

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