Mode Ⅲ 형을 가진 TDCB 알루미늄 폼에 대한 정적 파괴 거동
Static Fracture Behavior on TDCB Aluminum Foam with the Type of Mode Ⅲ
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초록
An aluminum foam is the super light metal which can be adjusted with the adhesive by using the joint method. In this study, the tapered double cantilever beams(TDCB) with the type of mode Ⅲ are manufactured with aluminum foam. The fracture toughness at the joint of the structure bonded with only a adhesive can be obtained. The static analyses are carried out and verified the results by the experiment. As the results of static analyses, the reaction forces ranged from 0.30 to 0.41 kN at all specimens are shown when the forced displacements are proceeded as much as 8 to 9 mm. The tapered double cantilever specimen for mode Ⅲ with the thickness of 55 mm is carried out by the static experiment representatively to verify the analysis results. As the results of analyses and experiments are compared with each other, there is a little bit of difference between these results. So, the simulation results of this study can be thought to be confirmed. It is thought that even the only analysis data omitting the extra experimental procedure can be verified in order to use the data practically. Through the result of this study, the mechanical properties at TDCB specimens with the type of mode Ⅲ can be understood.
Abstract
An aluminum foam is the super light metal which can be adjusted with the adhesive by using the joint method. In this study, the tapered double cantilever beams(TDCB) with the type of mode Ⅲ are manufactured with aluminum foam. The fracture toughness at the joint of the structure bonded with only a adhesive can be obtained. The static analyses are carried out and verified the results by the experiment. As the results of static analyses, the reaction forces ranged from 0.30 to 0.41 kN at all specimens are shown when the forced displacements are proceeded as much as 8 to 9 mm. The tapered double cantilever specimen for mode Ⅲ with the thickness of 55 mm is carried out by the static experiment representatively to verify the analysis results. As the results of analyses and experiments are compared with each other, there is a little bit of difference between these results. So, the simulation results of this study can be thought to be confirmed. It is thought that even the only analysis data omitting the extra experimental procedure can be verified in order to use the data practically. Through the result of this study, the mechanical properties at TDCB specimens with the type of mode Ⅲ can be understood.
참고문헌 (6)
- 최해규, "알루미늄 폼으로 된 DCB 모델의 피로해석에 관한 연구", 한국기계기술학회지, 14(6), pp.39~43 (2012), 한국기계기술학회
- 박성완, "ModeⅠ 하중에서의 에폭시계 접착제의 피로균열 진전특성", 한국기계기술학회지, 15(1), pp.5~13 (2013), 한국기계기술학회
- 김성수, "Study on the Fatigue Experiment of TDCB Aluminum Foam Specimen Bonded with Adhesive", International Journal of Precision Engineering and Manufacturing, 14(10), pp.1791~1795 (2013), 한국정밀공학회
- 방혜진, "접착제로 접합된 이중외팔보 알루미늄폼의 파괴 거동에 관한 연구", 대한기계학회논문집 A, 38(5), pp.521~526 (2014), 대한기계학회
- 최해규, "알루미늄 폼 복합재료로 된 접합된 DCB 시험편의 구조 해석에 관한 연구", 한국산학기술학회논문지, 13(4), pp.1488~1495 (2012), 한국산학기술학회[DOI]
- 최해규, "알루미늄 폼으로 된 이중외팔보 시험편의 파괴 거동에 관한 실험적 연구", 한국기계기술학회지, 14(5), pp.37~41 (2012), 한국기계기술학회
