• 제목/요약/키워드: Skin-core Debonding

검색결과 4건 처리시간 0.021초

Effect of core shape on debonding failure of composite sandwich panels with foam-filled corrugated core

  • Malekinejadbahabadi, Hossein;Farrokhabadi, Amin;Rahimi, Gholam H;Nazerigivi, Amin
    • Steel and Composite Structures
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    • 제45권3호
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    • pp.467-482
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    • 2022
  • One of the major failure modes in composite sandwich structures is the separation between skins and core. In this study, the effect of employing foam filled composite corrugated core on the skin/core debonding (resistance to separation between skin and core) is investigated both experimentally and numerically. To this aim, triangular corrugated core specimens are manufactured and compared with reference specimens only made of PVC foam core in terms of skin/core debonding under bending loading. The corrugated composite laminates are fabricated using the hand layup method. Also, the Vacuumed Infusion Process (VIP) is employed to join the skins to the core with greater quality. Utilizing an End Notched Shear (ENS) fixture, three point bending tests are performed on the manufactured sandwich composite panels. The results reveal that the resistance to separation capacity and flexural stiffness of sandwich composite has been increased about 170% and 76%, respectively by using a triangular corrugated core. The Cohesive Zone Model (CZM) with appropriate cohesive law in ABAQUS finite element software is used to model the progressive face/core interfaces debonding the difference between experimental and numerical results in predicting the maximum born load before the skin/core separation is about 6 % in simple core specimens and 3% in triangular corrugated core specimens.

GFRP-알루미늄 하니컴 하이브리드 적층판의 압축 및 굽힘 파괴거동과 음향방출해석 (Acoustic Emission Characteristics and Fracture Behaviors of GFRP-Aluminum Honeycomb Hybrid Laminates under Compressive and Bending Loads)

  • 이기호;구자욱;최낙삼
    • Composites Research
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    • 제22권6호
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    • pp.23-31
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    • 2009
  • 압축하중 및 굽힘하중을 받는 유리섬유플라스틱(GFRP) 표피/ 알루미늄 하니컴 코어(GF-AH) 하이브리드 복합재료의 음향방출(AE) 특성을 다양한 파괴과정과 연결시켜 연구하였다. 표피층 파괴, 표피/코어간의 계면박리, 하니컴 알루미늄 벽의 국부적인 소성항복 좌굴 및 셀벽간의 접착수지 박리와 같은 다양한 파괴모드가 하니컴 코어/GFRP표피 복합재를 이용한 AE주파수 분포 해석과 진폭분포 해석결과를 통해 분류되었다. 높은 진폭을 가진 AE 사상율의 분포는 셀벽 접착수지의 파괴, 표피층과 심층 사이의 박리및 미세파괴, 섬유파단에 대응하였으며 다른 피크 주파수의 분포는 알루미늄 셀벽의 소성변형, 셀벽간의 마찰로부터 발생한 것이다. 결론적으로 GF-AH 하이브리드 복합재료의 파괴거동 특성은 AE기법을 활용한 비파괴 평가를 통해 분석 가능하였다.

Effect of stacking sequence on the flexural and fracture properties of carbon/basalt/epoxy hybrid composites

  • Lim, Jae Il;Rhee, Kyong Yop;Kim, Hyun Ju;Jung, Dong Ho
    • Carbon letters
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    • 제15권2호
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    • pp.125-128
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    • 2014
  • In this study, the effect of stacking sequence on the flexural and fracture properties of carbon/basalt/epoxy hybrid composites was investigated. Two types of carbon/basalt/epoxy hybrid composites with a sandwich form were fabricated: basalt skin-carbon core (BSCC) composites and carbon skin-basalt core (CSBC) composites. Fracture tests were conducted and the fracture surfaces of the carbon/basalt/epoxy hybrid composites were then examined using scanning electron microscopy (SEM). The results showed that the flexural strength and flexural modulus of the CSBC specimen respectively were ~32% and ~245% greater than those of the BSCC specimen. However, the interlaminar fracture toughness of the CSBC specimen was ~10% smaller than that of the BSCC specimen. SEM results on the fracture surface showed that matrix cracking is a dominant fracture mechanism for the CSBC specimen while interfacial debonding between fibers and epoxy resin is a dominant fracture process for the BSCC specimen.

복합재 샌드위치 패널 발사관의 폭발충격 영향도 분석 (The Effect of Pyro Shock on Canister with Composite Sandwich Panel)

  • 최원홍
    • 한국소음진동공학회논문집
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    • 제26권6_spc호
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    • pp.667-673
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    • 2016
  • Canister with composite sandwich panel has been suggested owing to its higher stiffness and strength over a weight for square shaped canisters. The pyro shock induced by a short time explosion inside a canister is generally considered to be the most severe source of load affecting on the entire structure. Therefore, in this study, the approach and modeling method to identify the effect of pyro shock on canister with composite sandwich panel in a numerical way were mainly discussed. Moreover, the verification was implemented through comparison with test results.