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      PVC폼 코어 탄소섬유샌드위치 복합재의 모드Ⅰ 층간분리특성에 대한 실험적 분석

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      https://www.riss.kr/link?id=A106817597

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      다국어 초록 (Multilingual Abstract)

      The light weight composite materials have been replacing in high performance structures. The object of this study is to examine the effects of the initial crack location on the delamination in a PVC foam cored sandwich composite that is used for the strength improvement of structures. To analysis the effects of the initial crack location on the delamination, the thickness of fiber laminates were changed with three types. The ModeⅠ specimen was used for evaluating the fracture toughness and crack behaviors. The material used in the experiment is a commercial twill carbon prepreg in CFRP material and Airex in PVC foam core. Sandwich laminate composites are composed by PVC foam core layer between CFRP face sheets. The face sheets were fabricated as three types of 3, 5 and 8 plies. The initial cracks were located in a PVC form core and the interface of upper CFRP sheet. From the results, the crack initiation was affected with the location of the initial crack inserted in the PVC foam core. The initiation of the crack irstly affected by the initial crack insertion location, and the initial crack insertion at the center of the PVC foam showed a rapid progress. Among them, the lamination of CFRP with 8 plies made the most rapid progress. And the critical energy release rate was 0.02 kJ/m², which is the lowest value when the initial crack was inserted into the interface between a PVC foam core and CFRP laminated with 3 plies at face sheet. Meanwhile, the highest value of 1.70 kJ/m² was obtained when the initial crack was located at the center line of PCV foam in case of the 8 plies face sheets.
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      The light weight composite materials have been replacing in high performance structures. The object of this study is to examine the effects of the initial crack location on the delamination in a PVC foam cored sandwich composite that is used for the s...

      The light weight composite materials have been replacing in high performance structures. The object of this study is to examine the effects of the initial crack location on the delamination in a PVC foam cored sandwich composite that is used for the strength improvement of structures. To analysis the effects of the initial crack location on the delamination, the thickness of fiber laminates were changed with three types. The ModeⅠ specimen was used for evaluating the fracture toughness and crack behaviors. The material used in the experiment is a commercial twill carbon prepreg in CFRP material and Airex in PVC foam core. Sandwich laminate composites are composed by PVC foam core layer between CFRP face sheets. The face sheets were fabricated as three types of 3, 5 and 8 plies. The initial cracks were located in a PVC form core and the interface of upper CFRP sheet. From the results, the crack initiation was affected with the location of the initial crack inserted in the PVC foam core. The initiation of the crack irstly affected by the initial crack insertion location, and the initial crack insertion at the center of the PVC foam showed a rapid progress. Among them, the lamination of CFRP with 8 plies made the most rapid progress. And the critical energy release rate was 0.02 kJ/m², which is the lowest value when the initial crack was inserted into the interface between a PVC foam core and CFRP laminated with 3 plies at face sheet. Meanwhile, the highest value of 1.70 kJ/m² was obtained when the initial crack was located at the center line of PCV foam in case of the 8 plies face sheets.

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      참고문헌 (Reference)

      1 황우채, "경량화용 CFRP 단일 모자형 부재와 CFRP 이중 모자형 부재의 계면수 변화에 따른 정적압궤특성" 한국안전학회 26 (26): 20-25, 2012

      2 Y. S. Kim, "Study on Evaluation of Fracture Toughness in the Laminated Composites" 38 (38): 238-294, 2001

      3 K.R. Pradeep, "Interface fracture assessment on honeycomb sandwich composite DCB specimens" Elsevier BV 93 : 108-118, 2012

      4 V. Rizov, "Indentation study of foam core sandwich composite panels" Elsevier BV 69 (69): 95-102, 2005

      5 John Susainathan, "Experimental investigation of compression and compression after impact of wood-based sandwich structures" Elsevier BV 220 : 236-249, 2019

      6 O. Mociamn, "Experimental and numerical analyses of impact response of lightweight sandwich panels" 5 : 26634-26641, 2018

      7 Wentao He, "Effect of structural parameters on low-velocity impact behavior of aluminum honeycomb sandwich structures with CFRP face sheets" Elsevier BV 137 : 411-432, 2019

      8 G. S. Bir, "Computerized Method for Preliminary Structural Design of Composite for Two-and Three-Blade Rotors" NREL 2004

      9 Rodney McAdam, "Collaborative knowledge sharing in Composite New Product Development: An aerospace study" Elsevier BV 28 (28): 245-256, 2008

      10 F. Avilés, "Analysis of the sandwich DCB specimen for debond characterization" Elsevier BV 75 (75): 153-168, 2008

      1 황우채, "경량화용 CFRP 단일 모자형 부재와 CFRP 이중 모자형 부재의 계면수 변화에 따른 정적압궤특성" 한국안전학회 26 (26): 20-25, 2012

      2 Y. S. Kim, "Study on Evaluation of Fracture Toughness in the Laminated Composites" 38 (38): 238-294, 2001

      3 K.R. Pradeep, "Interface fracture assessment on honeycomb sandwich composite DCB specimens" Elsevier BV 93 : 108-118, 2012

      4 V. Rizov, "Indentation study of foam core sandwich composite panels" Elsevier BV 69 (69): 95-102, 2005

      5 John Susainathan, "Experimental investigation of compression and compression after impact of wood-based sandwich structures" Elsevier BV 220 : 236-249, 2019

      6 O. Mociamn, "Experimental and numerical analyses of impact response of lightweight sandwich panels" 5 : 26634-26641, 2018

      7 Wentao He, "Effect of structural parameters on low-velocity impact behavior of aluminum honeycomb sandwich structures with CFRP face sheets" Elsevier BV 137 : 411-432, 2019

      8 G. S. Bir, "Computerized Method for Preliminary Structural Design of Composite for Two-and Three-Blade Rotors" NREL 2004

      9 Rodney McAdam, "Collaborative knowledge sharing in Composite New Product Development: An aerospace study" Elsevier BV 28 (28): 245-256, 2008

      10 F. Avilés, "Analysis of the sandwich DCB specimen for debond characterization" Elsevier BV 75 (75): 153-168, 2008

      11 Stefano Bennati, "An enhanced beam-theory model of the asymmetric double cantilever beam (ADCB) test for composite laminates" Elsevier BV 69 (69): 1735-1745, 2009

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2022 평가예정 재인증평가 신청대상 (재인증)
      2020-01-01 학술지명변경 한글명 : 한국동력기계공학회지 -> 동력시스템공학회지
      외국어명 : Journal of the Korean Society for Power System Engineering -> Journal of Power System Engineering
      KCI등재
      2019-01-01 평가 등재학술지 유지 (계속평가) KCI등재
      2016-01-01 평가 등재학술지 유지 (계속평가) KCI등재
      2012-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2009-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2008-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2007-01-01 평가 등재후보학술지 유지 (등재후보1차) KCI등재후보
      2006-01-01 평가 등재후보학술지 유지 (등재후보1차) KCI등재후보
      2004-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.22 0.22 0.21
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.19 0.18 0.334 0.06
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