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NTIS 바로가기한국항공우주학회지 = Journal of the Korean Society for Aeronautical & Space Sciences, v.36 no.9, 2008년, pp.841 - 850
김중진 (경상대학교 기계항공공학부) , 성명수 (경상대학교 기계항공공학부) , 김홍주 (한국항공우주산업(주)) , 차봉근 (한국항공우주산업(주)) , 권진회 (경상대학교 항공기부품기술연구소) , 최진호 (경상대학교 항공기부품기술연구소)
Strength and failure of composite-to-aluminum rivetted, bonded, and rivet/bonding hybrid single-lap joints were investigated by experiment. A total of 82 joint specimens were tested with 3 different overlap lengths and 2 types of stacking sequence. FM73m adhesive film and NAS9308-4-03 rivet were use...
Baker A., Dutton S., and Kelly D., Composite Materials for Aircraft Structures, AIAA Education Series, 2004
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Owens, J. F. P., and Lee-Sullivan, P., "Stiffness Behaviour due to Fracture in Adhesively Bonded Composite-to-Aluminum Joints I. Theoretical Model", International Journal of Adhesion & Adhesive", Vol. 20, No. 1, 2000, pp. 39-45
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Kelly, G., "Load Transfer in Hybrid (Bond/Bolted) Composite Single-lap Joints", Composite Structures, Vol. 69, No. 1, 2005, pp. 35-43
Kelly, G., "Quasi-static Strength and Fatigue Life of Hybrid (Bond/Bolted) Composite Single-lap Joints", Composite Structures, Vol. 72, No. 1, 2006, pp. 112-129
FM73 Toughened Epoxy Film, Manufacturer's Data Sheet, Cytec Engineering Materials Ltd
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