• Composites Research
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• 제18권1호
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• pp.30-37
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• 2005

본 연구에서는 3점 굽힘 실험과 코어의 실제 형상을 모델링한 유한요소 시뮬레이션을 병행하여 외피층의 항복, 층간분리 코어의 전단 및 국부적 좌굴과 같은 다양한 파손모드를 고려한 하니컴 샌드위치 복합재료의 강도 특성과 변형거동을 검토하였다. 외피층과 하니컴 코어층 사이를 완전 접착한 시험편과 부분 층간분리 시험편을 대상으로 하니컴 코어의 셀 크기와 외피층 두께를 변화시켜 시험편의 굽힘 강성, 굽힘 강도. 굽힘 응력, 변형 및 파손 거동을 해석하였다. 결론적으로 하니컴 코어의 셀 크기와 외피층의 두께가 하니컴 샌드위치 복합재료의 굽힘 강성과 강도, 변형/파괴 거동에 주된 영향을 미쳤으며 코어의 셀 크기가 크고 외피층의 두께가 얇은 경우 굽힘 강도는 $30\~68\%$ 정도까지 저하됨을 알 수 있었다.

• 한국산업융합학회 논문집
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• 제20권2호
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• pp.133-140
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• 2017

This paper is a study of the central structural unit model of the sandwich core structure. The applied model is based on the honeycomb structure formed by the truss, the H-shaped honeycomb structure formed by adding the truss of H shape to the space of the center portion, and the honeycomb structure formed by the plate. Applied material property is AISI 304 stainless steel, which has cost effectiveness and easy to get near place. The truss diameter of the model is three different type: 1mm, 2mm and 3mm. ABAQUS software is obtained to do the analysis and applied test is quasi-static loading. Boundary conditions for the analysis are that vertical direction loading at top place without any rotation and bottom surface is fixed. The test results show that the H-truss model has the highest stiffness and yield strength. Therefore, it is hoped that more and more researching for the development of a unit model in sandwich core structure has been investigating and that the developed sandwich core model can be applied into various industrial fields such as mechanical or aerospace industries.

• Advances in aircraft and spacecraft science
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• 제6권2호
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• pp.169-187
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• 2019

This work presents a practical detailed finite element (FE) approach for the three-dimensional (3D) free-vibration analysis of actual aircraft and spacecraft-type lightweight and thin honeycomb sandwich panels. It consists of calling successively in $MATLAB^{(R)}$, via a developed user-friendly GUI, a detailed 3D meshing tool, a macrocommands language translator and a commercial FE solver($ABAQUS^{(R)}$ or $ANSYS^{(R)}$). In contrary to the common practice of meshing finely the faces and core cells, the proposed meshing tool represents each wall of the actual hexagonal core cells as a single two-dimensional (2D) 4 nodes quadrangularshell element or two 3 nodes triangular ones, while the faces meshes are obtained simply using the nodes at the core-faces interfaces. Moreover, as the same 2D FE interpolation type is used for meshing the core and faces, this leads to an automatic handling of their required FE compatibility relations. This proposed approach is applied to a sample made of very thin glass fiber reinforced polymer woven composite faces and a thin aluminum alloy hexagonal honeycomb core. The unknown or incomplete geometric and materials properties are first collected through direct measurements, reverse engineering techniques and experimental-FE modal analysis-based inverse identification. Then, the free-vibrations of the actual honeycomb sandwich panel are analyzed experimentally under different boundary conditions and numerically using different mesh basic cell shapes. It is found that this approach is accurate for the first few modes used for pre-design purpose.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2005년도 춘계학술대회 논문집
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• pp.251-256
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• 2005

This study was performed the heat transportation ratio of three types of the following sandwich panel by KS F 2278(2003) ; Type ${\sharp}1$ : Carbon/epoxy Aluminum Honeycomb and Balsa Core Sandwich Panel(Thickness : 37mm), Type ${\sharp}2$ : Carbon/epoxy Aluminum Honeycomb Core Sandwich Panel(Thickness : 57mm), and Type ${\sharp}3$ : Carbon/epoxy Aluminum Honeycomb Core Sandwich Panel(Thickness : 37mm). Also was performed the heat transportation of next three types of the following sandwich panel by KS F2277(2002) ; Type ${\sharp}4$ and ${\sharp}5$ : 27mm, and 35mm thick-Aluminum Honeycomb Sandwich Panels, and Type ${\sharp}6$ : 27mm thick-Foaming Aluminum Sandwich Panel. It is the larger area between the skin and core, the heat transportation ratio is the higher, and when it is composed of the hybrid composite structure, good insulation property was shown.

• Steel and Composite Structures
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• 제48권3호
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• pp.263-273
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• 2023

This paper investigates dynamic characteristics of a graphene nanoplatelets reinforced composite (GNPRC) sandwich doubly curved shell based on the first-order shear deformation theory (FSDT) and Hamilton's principle. The sandwich doubly curved shell is fabricated from a core made of honeycomb materials sandwiched by composite GNPs reinforced face-sheets. Effective materials properties of composite face-sheets are assumed to vary based on Halpin-Tsai micromechanical models and rule of mixture. Furthermore, the material properties of honeycomb core are estimated using Gibson's formula. The fundamental frequencies of the shell are computed with changes of main geometrical and material properties such as amount and distribution type of graphene nanoplatelets, side length ratio, thickness to length ratio of and side length ratio of honeycomb. The Navier's technique is presented to obtain responses. Accuracy and trueness of the present model and analytical solution is confirmed through comparison of the results with available results in literature. It is concluded that an increase in thickness to length ratio yields a softer core with lower natural frequencies. Furthermore, increase in height to length ratio leads to significant decrease in natural frequencies.

• 한국화재소방학회논문지
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• 제24권3호
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• pp.72-77
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• 2010

허니컴 코아 구조는 강성과 강도가 뛰어나 건축물의 내장재 등 많은 분야에서 활용되고 있다. 특히 허니컴 종이는 생산 단가가 낮으며 재활용이 가능하여 환경오염을 일으키지 않는다. 그러나, 종이 재료의 특성상 화재에 취약하여 난연화 할 필요가 있다. 본 연구에서는 방화문 내장재 및 포장재에 보편적으로 사용되는 허니컴 종이의 난연 처리 방법에 따른 난연 성능을 평가하였다. 연구 대상으로는 난연종이로 제작된 허니컴과 실험실에서 제작된 방염 필름을 부착한 허니컴, 난연제 함침을 통해 제작된 허니컴, 난연제 함침 후 방염 필름을 부착한 허니컴을 포함해 총 4종에 관한 난연 성능을 비교하였다. 그 결과, 난연제를 함침한 허니컴 종이가 가장 우수한 난연 능력을 보여주었으며, 방염 필름은 착화 시간 지연에는 효과가 있었으나 열방출률 및 연기발생률에 부정적인 영향을 미치는 것으로 확인되었다.

• Steel and Composite Structures
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• 제21권3호
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• pp.605-628
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• 2016

The energy absorption characteristics of diamond core sandwich cylindrical columns under axial crushing process depend greatly on the amount of material which participates in the plastic deformation. Both the single-objective and multi-objective optimizations are performed for columns under axial crushing load with core thickness and helix pitch of the honeycomb core as design variables. Models are optimized by multi-objective particle swarm optimization (MOPSO) algorithm to achieve maximum specific energy absorption (SEA) capacity and minimum peak crushing force (PCF). Results show that optimization improves the energy absorption characteristics with constrained and unconstrained peak crashing load. Also, it is concluded that the aluminum tube has a better energy absorption capability rather than steel tube at a certain peak crushing force. The results justify that the interaction effects between the honeycomb and column walls greatly improve the energy absorption efficiency. A ranking technique for order preference (TOPSIS) is then used to sort the non-dominated solutions by the preference of decision makers. That is, a multi-criteria decision which consists of MOPSO and TOPSIS is presented to find out a compromise solution for decision makers. Furthermore, local and global sensitivity analyses are performed to assess the effect of design variable values on the SEA and PCF functions in design domain. Based on the sensitivity analysis results, it is concluded that for both models, the helix pitch of the honeycomb core has greater effect on the sensitivity of SEA, while, the core thickness has greater effect on the sensitivity of PCF.

• 한국산학기술학회논문지
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• 제19권1호
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• pp.666-671
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• 2018

허니콤 판재(honeycomb panel)는 벌집 모양의 코어(core) 양쪽면에 표면판재를 부착시켜 만든 판재이다. 허니콤 판재는 비강도가 뛰어나며, 재료에 압축하중이 가해졌을 때 재료가 수차례의 좌굴을 반복하기 때문에 에너지 흡수성이 우수하여 내충격성이 요구되는 부위에 사용하기에 적합하다. 특히 최근에는 수송기기의 경량화에 대한 요구가 증가함에 따라 알루미늄 허니콤 판재를 자동차 및 고속전철 등의 차체 재료로 이용하려는 연구가 진행되고 있다. 이 밖에도 허니콤 판재는 흡음성과 평활성이 우수하며, 단열성과 내피로성도 우수하다. 연료 경제성을 증가시키기 위하여 알루미늄 합금 소재와 같은 경량 소재를 허니콤 판재 주 재료로 사용하여 무게를 감량시키는 것에 관한 연구를 진행 하였다.본 연구에서는 허니콤 판재의 설계기술, 알루미늄 허니콤 코어 및 허니콤 판재 제조 기술에 대한 연구를 수행하였으며, 또한 제조된 허니콤 판재의 각종 기계적 특성평가를 행하여 그 결과를 바탕으로 알루미늄 허니콤 판재의 제조 공정 설계, 판재 제작 및 특성 평가방안을 마련하였다. 연구결과 허니콤 판재의 우수한 에너지 흡수성은 코어 버클링의 반복에 기인하며 압축강도가 높을수록 접합면적당 강도 또한 높은 값을 나타내었다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2001년도 춘계학술대회 논문집
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• pp.740-743
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• 2001

Sandwich structure is widely used in various fields of industry due to its excellent strength and stiffness compared with weight. We studied the sandwich structure which has honeycomb core type. We are concerned about its buckling and bending stress with respect to its side length, thickness and the height ratio of its unit core. After obtaining the buckling critical load of unit core, we applied it to the sandwich structure to observe the bending behavior. When we compared the buckling with bending stress under buckling critical load, we observed that models of which length ratio of unit honeycomb core, A, is lower than 0.04 and the thickness of core, t, is thicker than 0.09 mm, is subjected to the ultimate stress by bending before buckling.

• 한국산학기술학회논문지
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• 제13권2호
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• pp.478-484
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• 2012

본 연구에서는 다공성 심재를 갖는 샌드위치 복합재료의 압축해석을 수행하였다. 알루미늄 폼 및 허니컴 코어 샌드위치 복합재료의 유한요소모델은 솔리드 요소를 적용하였다. 알루미늄 폼 코어의 경우에는 유효등가손상모델을 적용하였다. 면내 압축해석에서 알루미늄 폼 및 허니컴 코어 샌드위치의 압축 최대하중이 비슷했다. 그러나 알루미늄 허니컴 코어 샌드위치의 하중 지지구간이 더 길었다. 면외 압축에서는 알루미늄 허니컴 코어 샌드위치의 압축 최대하중이 알루미늄 폼 코어 샌드위치보다 높게 나왔다. 시뮬레이션 해석을 통하여 샌드위치 복합재료의 압축 거동을 얻을 수 있었다.