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      KCI등재 SCI SCIE SCOPUS

      Enhancement of the in-Plane Shear Properties of Carbon Fiber Composites Containing Carbon Nanotube Mats

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      https://www.riss.kr/link?id=A103920722

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      다국어 초록 (Multilingual Abstract)

      The in-plane shear property of carbon fiber laminates is one of the most important structural features ofaerospace and marine structures. Fiber-matrix debonding caused by in-plane shear loading is the major failuremode of carbon fiber composites because of the stress concentration at the interfaces. In this study, carbonnanotube mats (CNT mat) were incorporated in two different types of carbon fiber composites. For the case ofwoven fabric composites, mechanical interlocking between the CNTs and the carbon fibers increased resistanceto shear failure. However, not much improvement was observed for the prepreg composites as a result of incorporationof the CNT mats. The reinforcement mechanism of the CNT mat layer was investigated by a fractographicstudy using scanning electron microscopy. In addition, the CNT mat was functionalized by three differentmethods and the effectiveness of the functionalization methods was determined and the most appropriatefunctionalization method for the CNT mat was air oxidation.
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      The in-plane shear property of carbon fiber laminates is one of the most important structural features ofaerospace and marine structures. Fiber-matrix debonding caused by in-plane shear loading is the major failuremode of carbon fiber composites becau...

      The in-plane shear property of carbon fiber laminates is one of the most important structural features ofaerospace and marine structures. Fiber-matrix debonding caused by in-plane shear loading is the major failuremode of carbon fiber composites because of the stress concentration at the interfaces. In this study, carbonnanotube mats (CNT mat) were incorporated in two different types of carbon fiber composites. For the case ofwoven fabric composites, mechanical interlocking between the CNTs and the carbon fibers increased resistanceto shear failure. However, not much improvement was observed for the prepreg composites as a result of incorporationof the CNT mats. The reinforcement mechanism of the CNT mat layer was investigated by a fractographicstudy using scanning electron microscopy. In addition, the CNT mat was functionalized by three differentmethods and the effectiveness of the functionalization methods was determined and the most appropriatefunctionalization method for the CNT mat was air oxidation.

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      참고문헌 (Reference)

      1 E. Totry, 70 : 970-, 2010

      2 Y. Liang, 32 : 594-, 2013

      3 T. Saotome, 34 : 623-, 2011

      4 T. Saotome, 34 : 615-, 2011

      5 C. Thomsen, 85 : 5214-, 2000

      6 J. N. Coleman, 44 : 1624-, 2006

      7 P. C. Ma, 41 : 1345-, 2010

      8 Z. Spitalsky, 35 : 357-, 2010

      9 P. D. Bradford, 70 : 1980-, 2010

      10 Z. Spitalsky, 20 : 405702-, 2009

      1 E. Totry, 70 : 970-, 2010

      2 Y. Liang, 32 : 594-, 2013

      3 T. Saotome, 34 : 623-, 2011

      4 T. Saotome, 34 : 615-, 2011

      5 C. Thomsen, 85 : 5214-, 2000

      6 J. N. Coleman, 44 : 1624-, 2006

      7 P. C. Ma, 41 : 1345-, 2010

      8 Z. Spitalsky, 35 : 357-, 2010

      9 P. D. Bradford, 70 : 1980-, 2010

      10 Z. Spitalsky, 20 : 405702-, 2009

      11 Q. F. Cheng, 48 : 260-, 2010

      12 C. Fernández, 55 : 421-, 2013

      13 J. Cho, 56 : 685-, 2007

      14 H. S. Kim, 47 : 2779-, 2009

      15 H. S. Kim, 45 : 1109-, 2011

      16 S. U. Khan, 50 : 5265-, 2012

      17 박용빈, "Structural Analysis of a Composite Target-drone" 한국항공우주학회 12 (12): 84-91, 2011

      18 김한상, "Processing and Characterization of Carbon Nanotube Mat/Epoxy Composites" 대한금속·재료학회 17 (17): 697-704, 2011

      19 I. M. Daniel, "Engineering Mechanics of Composite Materials" Oxford University Press 100-106, 1994

      20 "ASTM standard D3518/D3518M, Standard Test Method for In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a ±45° Laminate"

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
      2009-12-29 학회명변경 한글명 : 대한금속ㆍ재료학회 -> 대한금속·재료학회 KCI등재
      2008-01-01 평가 SCI 등재 (등재유지) KCI등재
      2005-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2004-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2002-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 2.05 0.91 1.31
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      1.03 0.86 0.678 0.22
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