• 한국해양공학회지
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• 제16권6호
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• pp.55-59
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• 2002

Delamination means that cracking occurs on the interface layer between composite laminates. In this paper, to predict the delamination growth in composite laminates subjected to low-velocity impact, the unit load method was introduced, and an eighteen-node 3-D finite element analysis, based on assumed strain mixed formulation, was conducted. Strain energy release rate, necessary to determine the delamination growth, was calculated by using the virtual crack closure technique. The unit load method saves the computation time more than the re-meshing method. The virtual crack closure technique enables the strain energy release rate to be easily calculated, because information of the singular stress field near the crack tip is not required. Hence, the delamination growth in composite laminates that are subjected to low-velocity impact can be efficiently predicted using the above-mentioned methods.

• Structural Engineering and Mechanics
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• 제28권3호
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• pp.335-352
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• 2008

Continuous operation of test and measurement is a new operating technique in the petroleum exploitation, which combines perforation with test and measurement effectively. In order to measure the original pressure of stratum layer exactly and prevent testing instrument from being impaired or damaged, a suitable shock absorber is urgently necessary to research. Based on the attempt on the FEM analysis and experiment research, a new shock absorber is designed and discussed in this paper. 3D finite element model is established and simulated accurately by LS-DYNA, the effect and the dynamic character of the shock absorber impact by half sinusoidal pulse force under the main lobe frequency are discussed both on theoretics and experiment. It is shown that the new designed shock absorber system has good capability of shock absorption for the impact load.

• Structural Engineering and Mechanics
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• 제36권6호
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• pp.729-744
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• 2010

There is world wide concern for safety of nuclear power installations after the terrorist attack on World Trade Center in 2001 and several other civilian structures in the last decade. The nuclear containment structure in many countries is a double shell structure (outer shell a RCC and inner a prestressed concrete). The outer reinforced concrete shell protects the inner shell and is designed for external loading like impact and blast. A comparative study of non-linear response of reinforced concrete nuclear containment cylindrical shell subjected to impact of an aircraft (Phantom) and explosion of different amounts of blast charges have been presented here. A material model which takes into account the strain rate sensitivity in dynamic loading situations, plastic and visco-plastic behavior in three dimensional stress state and cracking in tension has been developed earlier and implemented into a finite element code which has been validated with published literature. The analysis has been made using the developed software. Significant conclusions have been drawn for dissimilarity in response (deflections, stresses, cracks etc.) of the shell for impact and blast loading.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 추계학술대회논문집
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• pp.390-393
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• 2005

In this study, examined heavy-weight floor impact sound to rahmen structure(steel reinforced concrete structure) and bearing-wall structure(box frame type structure) that have slab thickness of 4 form at a standard laboratory through noise and vibration measured. The results of ANSYS modeling of structures was predicted that the nature natural frequency increased according to change of thickness of each slab by finite element analysis, and acceleration value decreased. Rahmen structures compares with bearing-wall structure, nature frequency was predicted low. Measurement results of natural frequency and acceleration level for structures at a standard laboratory, tendency department such as ANSYS modeling appeared. Rahmen structures appeared that reduction effect is less in Acceleration level and heavy impact sound transmission level comparing with bearing-wall structure.

• 한국산학기술학회논문지
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• 제19권4호
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• pp.111-116
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• 2018

본 논문은 시스템 에어컨 실외기 포장품의 낙하충격해석 및 시험검증을 수행한 내용을 다룬다. 포장은 낙하충격으로 부터 제품을 보호할 수 있도록 충격에너지를 흡수할 수 있는 완충재질과 이를 제품에 고정하기 위한 부재로 구성되는데 작은 부피로 충분한 완충성능을 발휘하는 포장 설계를 위해서는 충격 시 제품에 가해지는 충격가속도 등을 정확히 평가하는 것이 필수적이다. 본 논문에서는 외연적 시간적분을 활용하는 유한요소해석 기법을 활용하여 실외기 포장품의 낙하충격해석을 수행하였다. 정확한 해석을 위한 해석모델 구축, 재료 시험을 통한 데이터 획득 및 재료 모델의 선정, 신뢰성 있는 해석 데이터 확보를 위한 계측 센서의 모델링 등이 수행되었으며 이렇게 구해진 해석데이터와 시험으로 구해진 가속도 및 변형률 시간이력을 비교하였다. 해석모델에 반영된 감쇄계수 등의 오차로 인하여 대체로 해석결과가 시험 결과에 비해 충격 가속도 및 변형률을 크게 예측하고 있으나 전체적인 데이터의 경향과 낙하 방향의 충격가속도는 정확하게 계산되었다. 이에 본 연구에 사용된 모델 및 해석기법을 에어컨 실외기 포장 설계에 활용할 수 있음을 확인하였다.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2003년도 춘계학술대회 논문집
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• pp.734-739
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• 2003

When a train moves on rails, wheel and rail vibrate to produce contact noise and contact force. The former results in airborne noise and the latter transmits through bogie and excites carbody to generate structure borne noise. In this paper, wheel vibration is studied by theoretical and experimental approaches. Theoretical analysis is performed by finite element method and experimental analysis is performed by impact test. Using modal analysis and model tunning, we could have good agreement between the two approaches.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 춘계학술발표대회 논문집
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• pp.67-70
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• 2004

An investigation was performed to study the impact damage of the laminated composite plates caused by a low- velocity foreign object with multi-scale modeling based on the concepts of Direct Numerical Simulation (DNS)[4]. In the micro-scale part, we discretize the composite plates through separate modeling of fiber and matrix for the local microscopic analysis. A micro-scalemodel was developed for predicting the initiation of the damage and the extent of the final damage as a function of material properties, laminate configuration and the impactor's mass, etc. Anda macro-scale model was developed for description of global dynamic behavior. The connection betweenmicroscopic and macroscopic is implemented by the tied interface constraints of LS-DYNA contact card. A transient dynamic finite element analysis was adopted for calculating the contact force history and the stresses and strains inside the composites during impact resulting from a point-nose impactor. The low-velocity impact events such as contact force, deformation, etc. are simulated in the macroscopic sense and the impact damages, fiber-breakage, matrix cracking and delamination etc. are examined in the microscopic sense.

• Steel and Composite Structures
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• 제38권6호
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• pp.717-737
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• 2021

A theoretical energy-based model to capture the mechanical response of thick woven composite laminates, which are used in such applications as maritime or aerospace, to high-velocity impact was developed. The dependences of the impact phenomenon on material and geometrical parameters were analysed making use of the Vaschy-Buckingham Theorem to provide a non-dimensional framework. The model was divided in three different stages splitting the physical interpretation of the perforation process: a first where different dissipative mechanisms such as compression or shear plugging were considered, a second where a transference of linear momentum was assumed and a third where only friction took place. The model was validated against experimental data along with a 3D finite element model. The numerical simulations were used to validate some of the new hypotheses assumed in the theoretical model to provide a more accurate explanation of the phenomena taking place during a high-velocity impact.

• 대한기계학회논문집A
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• 제36권6호
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• pp.699-705
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• 2012

안전벨트의 역할은 차량 충돌이 발생했을 때 운전자를 보호하는 것이다. 그러나 강한 충돌이 발생하게 되면 운전자가 안전벨트에서 미끄러지게 되어 강한 충격을 받는다. 그러므로 이러한 현상을 방지하기 위해 새로운 안전벨트의 개발이 필요하다. 이 연구에서는 새로운 개념의 안전벨트인 Dynamic Locking Tongue(DLT)을 개발하였다. DLT장치는 강한 충돌이 발생했을 때 벨트(Webbing)가 안전벨트에서 미끄러지지 않게 하여 운전자의 피해를 줄여주는 장치이다. DLT장치 개발은 동역학 해석 프로그램인 SAMCEF를 이용하였다. 우선 DLT장치의 유한요소모델을 생성하였다. 그리고 실제 시험방법과 유사한 환경을 만들어 테스트를 해보았다. 이를 통해 DLT장치의 무게와 응력를 구할 수 있다. DLT장치의 최소 강도와 무게를 구하기 위해 반응 표면 분석법을 이용하여 DLT장치의 형상을 최적화하였다. 최적화된 DLT장치를 구조 해석을 통해 신뢰성을 검증하였다.

• 콘크리트학회논문집
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• 제26권3호
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• pp.393-400
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• 2014

구조물은 사고 혹은 테러에 의한 공격 등과 같은 차량에 의한 충돌에 노출되어 있으며, 차량 충격이 구조물의 주요 기둥에 발생 할 경우 구조물 전체가 연쇄붕괴로 인하여 붕괴 할 수 있다. 이 연구에서는 차량 충격하중을 받는 강재 기둥과 콘크리트 기초 상부 접합부의 거동 및 보강방법에 관하여 분석하였다. 충돌해석을 위하여 모델링 된 단일 강재 기둥의 크기와 기둥이 받는 축 하중의 양은 일반적인 3층, 6 m길이의 3경간 구조물의 1층에 위치한 기둥으로 가정하였다. 또한 충돌해석에 사용한 8톤 트럭은 미국 NCAC(National Crash Analysis Center)에서 제공한 모델을 사용하였다. 충돌 해석은 상용 유한요소 프로그램인 LS-DYNA를 사용하였으며 차량 충돌해석 해석 결과, 충격하중을 받는 기둥은 기초 상부 앵커볼트 및 접합부 형태에 큰 영향을 받는 것으로 나타났다.