• 한국산학기술학회논문지
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• 제15권10호
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• pp.5963-5967
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• 2014

본 자동차 충돌사고는 인간이 자동차 문명을 발전시킨 이래 누려온 편의성의 대가이기 때문에 많은 사람들이 충돌사고 시 승객의 사망과 상해를 기술적으로 감소시키기 위해 여러 가지 노력을 기울여 왔다. 도로교통공단 통계자료에 따르면 승용차 충돌사고로 인한 사망자 충 측면충돌사고에 의한 사망자가 정면충돌사고의 사망자보다 많다. 자동차 설계자들은 이에 대응하기 위해 도어 내부에 임팩트 빔(Impact Beam)과 임팩트 프레임(Impact Frame)이라는 보강재를 추가시켜 왔다. 이러한 보강재 개발을 위해 충돌실험은 필수적이다. 충돌실험의 경우 많은 비용과 시간이 소모되게 된다. 본 연구는 임팩터를 떨어뜨려 충격량과 변형량을 얻을 수 있는 실험장치 개발이 목적이다. 경제적 비용을 줄일 수 있는 이상적인 실험장치 구성을 제시하고, 수치해석 값과 실험결과 값을 비교 분석한 결과 충돌 시작 후 3.5E-3sec에서 각각 3.49E-3, 3.99E-3의 변형량을 나타냈다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집A
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• pp.153-158
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• 2000

Nuclear reactor pressure vessel should be safety even in the case that hypothetical defects with allowable size are in vessel. Therefore, the materials should have excellent fracture resistance characteristics. The purpose of this study is to analyze the results of preirradiation baseline test of nuclear pressure vessel for Yonggwang Unit 5/6. In experiments, drop weight tests and impact tests are carried out to obtain nil-ductility transition reference temperature, $RT_{NDT}$ and static and dynamic fracture toughness tests are performed to compare with $K_{IR}$ curve in accordance with ASME Sec.III. The test results show that the materials had sufficiently fracture resistance characteristics for 40 years of design life.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 추계학술발표대회 논문집
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• pp.65-68
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• 2004

A new multifunctional sandwich composite was investigated in this paper. The honeycomb core of this composite was filled with viscoelastic material in order to obtain an improved impact performance. The fillings in the honeycomb cells was hoped to provide the act of energy dissipation in this combined material system. Low-velocity drop-weight test was set up to the specimens with various stacked carbon/epoxy laminate facesheets, $[0/90]_{4s},\;[0/45/-45/90]_{2s}$. Load and energy history were checked and compared for the both groups of specimens, with and without rubber fillings. Further, the damaged faces were inspected visually by ultrasonic C-scan.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 추계학술발표대회 논문집
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• pp.31-34
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• 2005

For the damage tolerance improvement of conventional laminated composites, stitching process has been utilized for providing through-thickness reinforcements. 2D prefonl1S were stacked with S-2 glass plain weave, and 3D preforms were fabricated using the stitching process. For the matrix system, epoxy and phenol resins were considered. To examine the damage resistance performance the low velocity drop weight impact test has been carried out, and the impact damage was examined by scanning image. CAI (Compressive After Ih1paet) tests were also conducted to evaluate residual compressive strength. Compared with 2D epoxy composites, 2D phenol composites showed drastic reduction in the compressive strength prior to impact because of the higher contents of voids. The damage area of 2D phenol composites were also larger than that of 2D epoxy composites. However, by introducing the stitching, the damage area of 3D phenol composites was reduced by 60%, while the CAI strength improvement was negligible.

• Structural Engineering and Mechanics
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• 제7권4호
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• pp.387-400
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• 1999

Damage detection in civil engineering structures using the change in dynamic system parameters has gained a lot of scientific interest during the last decade. By repeating a dynamic test on a structure after a certain time of use, the change in modal parameters can be used to quantify and qualify damages. To be able to use the modal parameters confidentially for damage evaluation, the effect of other parameters such as excitation type, ambient conditions,... should be considered. In this paper, the influence of excitation type on the dynamic system parameters of a highway prestressed concrete bridge is investigated. The bridge, B13, lies between the villages Vilvoorde and Melsbroek and crosses the highway E19 between Brussels and Antwerpen in Belgium. A drop weight and ambient vibration are used to excite the bridge and the response at selected points is recorded. A finite element model is constructed to support and verify the dynamic measurements. It is found that the difference between the natural frequencies measured using impact weight and ambient vibration is in general less than 1%.

• Advances in concrete construction
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• 제15권3호
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• pp.161-170
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• 2023

Ultra-high-performance concrete (UHPC) is produced using high amount of cementitious materials, very low water/cementitious materials ratio, fine-sized fillers, and steel fibers. Due to the dense microstructure of UHPC, it possesses very high strength, elasticity, and durability. Besides that, the UHPC exhibits high ductility and fracture toughness due to presence of fibers in its matrix. While the high ductility of UHPC allows it to undergo high strain/deflection before failure, the high fracture toughness of UHPC greatly enhances its capacity to absorb impact energy without allowing the formation of severe cracking or penetration by the impactor. These advantages with UHPC make it a suitable material for construction of the structural members subjected to special loading conditions. In this research work, the UHPC mixtures having three different dosages of steel fibers (2%, 4% and 6% by weight corresponding to 0.67%, 1.33% and 2% by volume) were characterized in terms of their mechanical properties including facture toughness, before using these concrete mixtures for casting the slab specimens, which were tested under high-energy impact loading with the help of a drop-weight impact test setup. The effect of fiber content on the impact energy absorption capacity and central deflection of the slab specimens were investigated and the equations correlating fiber content with the energy absorption capacity and central deflection were obtained with high degrees of fit. Finite element modeling (FEM) was performed to simulate the behavior of the slabs under impact loading. The FEM results were found to be in good agreement with their corresponding experimentally generated results.

• 한국항공우주학회지
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• 제38권9호
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• pp.862-868
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• 2010

국내에서 미국과 상호항공안전협정 체결을 위해 소형 항공기를 개발 중이다. 연구 대상 항공기는 경량화를 위하여 전기체 복합재료가 적용되었다. 그러나 복합재 구조는 충격 손상에 취약하다. 따라서 본 연구에서는 항공기 복합재 구조의 손상 평가 및 유지 보수 기법 연구를 수행하였다. 탄소/에폭시 UD 라미네이트와 탄소/에폭시 패브릭 스킨-허니컴코어 샌드위치 복합재 라미네이트의 손상은 중량 낙하식 충격 시험기를 활용하여 모사되었으며 손상된 시편은 손상 부위 제거 후 외부 패치 적용 방안을 적용하여 수리하였다. 손상 전 시편, 손상 후 시편, 유지 보수된 시편의 압축 강도 시험 및 해석 결과를 비교하였다. 그리고 마지막으로 유지 보수 후 강도 복원 능력이 평가되었다.

• Advances in concrete construction
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• 제15권1호
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• pp.23-39
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• 2023

One of the important problems of concrete placing is the concrete compaction, which can affect the strength, durability and apparent quality of the hardened concrete. Therefore, vibrating operations might be accompanied by much noise and the need for training the involved workers, while inappropriate functioning can result in many problems. One of the most important methods to solve these problems is to utilize self-compacting cementitious composites instead of the normal concrete. Due to their benefits of these new materials, such as high tensile, compressive, and flexural strength, have drawn the researchers' attention to this type of cementitious composite more than ever. In this experimental investigation, six mixing designs were selected as a base to acquire the best mechanical properties. Moreover, forty-eight rectangular composite panels with dimensions of 300 mm × 400 mm and two thickness values of 30 mm and 50 mm were cast and tested to compare the flexural and impact energy absorption. Steel fibers with volume fractions of 0%, 0.5% and 1% and with lengths of 25 mm and 50 mm were imposed in order to prepare the required cement composites. In this research, the composite panels with two thicknesses of 30 mm and 50 mm, classified into 12 different groups, were cast and tested under three-point flexural bending and repeated drop weight impact test, respectively. Also, the examination and comparison of flexural energy absorption with impact energy absorption were one of the other aims of this research. The obtained results showed that the addition of fibers of longer length improved the mechanical properties of specimens. On the other hand, the findings of the flexural and impact test on the self-compacting composite panels indicated a stronger influence of the long-length fibers.

• 항공우주기술
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• 제12권1호
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• pp.213-220
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• 2013

국가우주개발계획에 따라 2020년 이후 한국형 달탐사선이 발사될 예정이다. 달탐사선은 무인 경량화모델로 달궤도선과 달착륙선 2종을 개발할 계획이다. 달탐사선의 구조체는 발사 및 궤도하중, 착륙하중을 견딜 수 있는 구조적 안정성과 탑재장비의 장착공간을 제공할 뿐만 아니라 발사체의 탑재능력을 고려하여 가볍게 설계되어야 한다. 이를 위해 달탐사선 구조체의 개발과 관련된 핵심기술의 선행개발이 요구된다. 특히, 달착륙선의 경우 착륙선이 달 지면에 안전하게 착륙할 수 있게 해주는 착륙장치의 개발기술이 필수적이다. 본 논문에서는 달착륙선 지상시험모델 구조체의 설계, 제작, 시험을 포함한 개발내용을 다룬다.

• Steel and Composite Structures
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• 제46권4호
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• pp.525-538
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• 2023

This paper focuses on the energy absorption of lattice core sandwich structures of different configurations. The diamond lattice unit cell, which has been extensively investigated for energy absorption applications, is the starting point for this research. The energy absorption behaviour of sandwich structures with an expanded metal sheet as the core is investigated at low-velocity impact loading. Numerical simulations were carried out using ABAQUS/EXPLICIT and the results were thoroughly compared with the experimental results, which indicated desirable accuracy. A parametric analysis, using a Box-Behnken design (BBD), as a method for the design of experiments (DOE), was performed. The samples fabricated in three levels of parameters include 0.081, 0.145, and 0.562 mm² Cell sizes, and 0, 45, and 90-degree cell orientation, which were investigated. It was observed from experimental data that the angle of cells orientation had the highest degree of influence on the specific energy absorption. The results showed that the angle of cells orientation has been the most influential parameter to increase the peak forces. The results from using the design expert software showed the optimal specific energy absorption and peak force to be 1786 J/kg and 26314.4 N, respectively. The obtained R2 values and normal probability plots indicated a good agreement between the experimental results and those predicted by the model.