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      KCI등재 SCIE

      Experiment and Analysis Verification of Shearing Fracture Characteristic of Tapered Double Cantilever Beam with Aluminum Foam

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      https://www.riss.kr/link?id=A103721973

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      다국어 초록 (Multilingual Abstract)

      In this study, mode II(sliding) adhesive strengths of tapered double-cantilever beam (TDCB) specimens of aluminum foams bonded with adhesives were evaluated by finite element analysis. Models were fabricated for testing, and their length and thickness...

      In this study, mode II(sliding) adhesive strengths of tapered double-cantilever beam (TDCB) specimens of aluminum foams bonded with adhesives were evaluated by finite element analysis. Models were fabricated for testing, and their length and thickness were 200 mm and 25 mm, respectively, while the angles between the adhesive layers and the horizontal direction for models (a), (b), and (c) were 8o, 10o, and 12o, respectively. The joint adhesive method was applied to the models that were made of Al-SAF40, aluminum foam. To generate the crack in shear direction, one end of the loaded block was restrained with a frictionless support while the other end of the loaded block was set to be displaced at the rate of 10 mm/min in the adhesive layer. The analysis and comparison result between the 3 different models revealed that the larger the tilt angle θ of sliding mode was, the larger the maximum load became, while the time to reach the maximum load and the time taken until the load disappeared were shorter as the value increased in the displacement-force reaction curve. This study can be applied to real structures with tapered contact surfaces by analyzing fracture behaviors and characteristics of composite materials such as aluminum foams bonded with adhesives.

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      참고문헌 (Reference)

      1 Blackman, B. R. K., "The Failure of Fibre Composites and Adhesively Bonded Fibre Composites under High Rates of Test" 31 (31): 4467-4477, 1996

      2 Blackman, B. R. K., "The Calculation of Adhesive Fracture Energies in Mode I: Revisiting the Tapered Double Cantilever Beam (TDCB)Test" 70 (70): 233-248, 2003

      3 김성수, "Study on the Fatigue Experiment of TDCB Aluminum Foam Specimen Bonded with Adhesive" 한국정밀공학회 14 (14): 1791-1795, 2013

      4 Paul, A., "Strain Rate Sensitivity of a Closed-Cell Aluminum Foam" 281 (281): 1-7, 2000

      5 Hojo, M., "Modes I and II Interlaminar Fracture Toughness and Fatigue Delamination of CF/Epoxy Laminates with Self-Same Epoxy Interleaf" 28 (28): 1154-1165, 2006

      6 Ohno, N., "Long-Wave Buckling of Elastic Square Honeycombs Subject to In-Plane Biaxial Compression" 46 (46): 1697-1713, 2004

      7 Shokrieh, M., "Influence of Curved Delamination Front on Toughness of Multidirectional DCB Specimens" 94 (94): 1359-1365, 2012

      8 Zhang, Y. J., "FEM Analyses for Influences of Stress-Chemical Solution on THM Coupling in Dual-Porosity Rock Mass" 19 : 1138-1147, 2012

      9 한문식, "Experimental Study on the Fatigue Crack Propagation Behavior of DCB Specimen with Aluminum Foam" 한국정밀공학회 14 (14): 1395-1399, 2013

      10 Nakai, Y., "Effects of Loading Frequency and Environment on Delamination Fatigue Crack Growth of CFRP" 24 (24): 161-170, 2002

      1 Blackman, B. R. K., "The Failure of Fibre Composites and Adhesively Bonded Fibre Composites under High Rates of Test" 31 (31): 4467-4477, 1996

      2 Blackman, B. R. K., "The Calculation of Adhesive Fracture Energies in Mode I: Revisiting the Tapered Double Cantilever Beam (TDCB)Test" 70 (70): 233-248, 2003

      3 김성수, "Study on the Fatigue Experiment of TDCB Aluminum Foam Specimen Bonded with Adhesive" 한국정밀공학회 14 (14): 1791-1795, 2013

      4 Paul, A., "Strain Rate Sensitivity of a Closed-Cell Aluminum Foam" 281 (281): 1-7, 2000

      5 Hojo, M., "Modes I and II Interlaminar Fracture Toughness and Fatigue Delamination of CF/Epoxy Laminates with Self-Same Epoxy Interleaf" 28 (28): 1154-1165, 2006

      6 Ohno, N., "Long-Wave Buckling of Elastic Square Honeycombs Subject to In-Plane Biaxial Compression" 46 (46): 1697-1713, 2004

      7 Shokrieh, M., "Influence of Curved Delamination Front on Toughness of Multidirectional DCB Specimens" 94 (94): 1359-1365, 2012

      8 Zhang, Y. J., "FEM Analyses for Influences of Stress-Chemical Solution on THM Coupling in Dual-Porosity Rock Mass" 19 : 1138-1147, 2012

      9 한문식, "Experimental Study on the Fatigue Crack Propagation Behavior of DCB Specimen with Aluminum Foam" 한국정밀공학회 14 (14): 1395-1399, 2013

      10 Nakai, Y., "Effects of Loading Frequency and Environment on Delamination Fatigue Crack Growth of CFRP" 24 (24): 161-170, 2002

      11 Batra, R. C., "Development of Shear Bands in Dynamic Plane Strain Compression of Depleted Uranium and Tungsten Blocks" 16 (16): 375-395, 1995

      12 "BS 7991:2001, Determination of the Mode I Adhesive Fracture Energy, GIC, of Structural Adhesives using the Double Cantilever Beam (DCB) and Tapered Double Cantilever Beam (TDCB)Specimens"

      13 Aymerich, F., "Analysis of the Effect of Stitching on the Fatigue Strength of Single-Lap Composite Joints" 66 (66): 166-175, 2006

      14 Michailidis, N., "An Imagebased Reconstruction of the 3D Geometry of an Al Open-Cell Foam and FEM Modeling of the Material Response" 42 (42): 142-147, 2010

      15 Öchsner, A., "A New Evaluation Procedure for the Butt-Joint Test of Adhesive Technology:Determination of the Complete Set of Linear Elastic Constants" 27 (27): 703-711, 2007

      16 Adams, R. D., "A Critical Assessment of the Block Impact Test for Measuring the Impact Strength of Adhesive Bonds" 16 (16): 61-71, 1996

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      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
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      2005-05-30 학술지명변경 한글명 : 한국정밀공학회 영문논문집 -> International Journal of the Korean of Precision Engineering KCI등재후보
      2005-05-30 학술지명변경 한글명 : International Journal of the Korean of Precision Engineering -> International Journal of Precision Engineering and Manufacturing
      외국어명 : International Journal of the Korean of Precision Engineering -> International Journal of Precision Engineering and Manufacturing
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