• 한국항공우주학회지
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• 제33권5호
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• pp.87-92
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• 2005

본 논문에서는 스마트무인기 콘솔구조의 설계개념을 소개하고, 장비의 안전성을 평가하기 위하여 충격과 진동에 대한 국방 환경시험규격을 적용하여 수치해석을 통한 주파수 응답스펙트럼을 분석하였다. 콘솔의 설계개념은 형상설계와 공학설계로 크게 분류된다. 형상설계는 콘솔의 운용성을 높이기 위한 인체공학규격을 기초로 하며, 공학설계는 충격과 진동에 대한 내구성을 높이기 위한 설계이다. 수치해석은 유한요소법을 통해 수행되었으며, 해석결과 콘솔에 설치된 6개의 탄성스프링은 충격과 진동에 대하여 충분한 감쇠를 보임이 확인되었다.

• 한국산학기술학회논문지
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• 제10권10호
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• pp.2583-2588
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• 2009

본 논문에서는 반정현파 형태의 충격을 받는 HDD에 대한 충격해석을 수행하고, 그 타당성을 실험적으로 검증하였다. 일반적으로 센서를 이용한 제품의 충격실험을 통해서는 제한적인 정보만을 얻을 수 있지만, 컴퓨터를 이용한 해석기술은 제품의 파손현상을 규명하는데 필요한 보다 광범위하고 상세한 정보를 제공할 수 있는 장점을 가진다. 하지만, 이러한 해석결과는 여러 요인들에 따라 매우 민감하기 때문에 그 타당성을 검증하는 것이 중요하다. 따라서 본 연구에서는 200G/1ms의 전자기 충격실험과 300G/2ms의 낙하충격실험을 통하여 HDD의 조립단계별로 LS-DYNA를 이용한 유한요소해석의 신뢰성을 검증하였다.

• Structural Engineering and Mechanics
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• 제53권1호
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• pp.73-87
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• 2015

In case of aircraft impact on nuclear containment structures, the initial kinetic energy of the aircraft is transferred and absorbed by the outer containment, may causing either complete or partial failure of containment structure. In the present study safety analysis of BWR Mark III type containment has been performed. The total height of containment is 67 m. It has a circular wall with monolithic dome of 21m diameter. Crash analysis has been performed for fighter jet Phantom F4. A normal hit at the crown of containment dome has been considered. Numerical simulations have been carried out using finite element code ABAQUS/Explicit. Concrete Damage Plasticity model have been incorporated to simulate the behaviour of concrete at high strain rate, while Johnson-Cook elasto-visco model of ductile metals have been used for steel reinforcement. Maximum deformation in the containment building has reported as 33.35 mm against crash of Phantom F4. Deformations in concrete and reinforcements have been localised to the impact region. Moreover, no significant global damage has been observed in structure. It may be concluded from the present study that at higher velocity of aircraft perforation of the structure may happen.

• 한국강구조학회 논문집
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• 제24권4호
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• pp.399-410
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• 2012

본 연구에서는 실험적 모드해석 기법을 이용하여 캔틸레버 및 양단고정 직사각형 적층복합판의 동적 테스트가 수행되었다. 균열 성장으로 인한 손상평가를 위하여 적층복합판에 인위적인 단계별 손상(균열)을 가하였으며, 충격해머 모드실험에 의해 얻어진 주파수응답함수(FRF), MAC(Modal Assurance Criterion) 값 및 모드매개변수(진동수, 모드형상, 감쇠비)의 변화를 분석하였다. 각 단계별 손상에 대한 적층복합판의 실험적 모드매개변수를 검증하기 위하여 유한요소해석으로부터 구한 고유진동수와 모드형상을 비교하였다. 손상은 벤치마크로서의 유한요소모델을 보정하는 과정으로부터 얻게 되는 적층복합판의 기하학적 특성 및 구조적 거동의 변화를 통하여 평가될 수 있음을 보여주었다.

• Composites Research
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• 제35권2호
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• pp.61-68
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• 2022

복합재료는 비강도, 비강성 및 내부식성 등이 우수하여 항공우주산업뿐만 아니라 다양한 산업에서 사용되고 있다. 그러나 복합재료는 충격에 취약하고 이러한 충격은 복합 재료 내부의 균열 형성과 균열 성장으로 이어져 구조 파단의 원인이 된다. 본 논문에서는 음향 방출 신호 및 유한요소해석(Finite element analysis, FEA)을 이용하여 복합재 적층판의 Mode I 파괴 모드의 특성을 분석하였다. DCB 시험은 탄소/에폭시 적층판의 Mode I 파괴 특성을 분석하기 위하여 수행되었고 시편의 파괴에 의해서 발생되는 탄성파를 측정하기 위하여 시편에 음향 방출 센서를 부착하였다. 누적 음향 방출 에너지와 균열 선단 위치의 관계를 이용하여 시편의 파괴 인성(Fracture toughness, G_I)을 계산하였다. 계산된 파괴 인성 값을 유한요소모델에 적용하여 해석을 수행하였고 하중-변위 곡선 및 균열 길이-변위 곡선을 통하여 DCB 시험 결과와 비교/분석하였다. 유한요소해석 및 DCB 시험의 결과가 잘 일치함을 보였다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.831-836
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• 2000

In this study, the Rayleigh inextensional theory and extensional theory for thin shells was employed to predict the natural frequencies of the hemi-spherical shell with free and simply. supported boundary condition. The frequencies and mode shapes from theoretical calculation were compared with those of commercial finite element code, ANSYS. In order to validate the theory, modal test was also performed by impact test and FFT analysis. Modal test and FEM analysis of the free, simply supported and clamped boundary condition was also carried out.

• Nuclear Engineering and Technology
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• 제32권2호
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• pp.180-190
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• 2000

In this study, nonlinear analyses of prestressed concrete(PSC) test beams for inservice inspection of prestressed concrete containments for CANDU nuclear power plants are presented. In the analysis the material nonlinearities of concrete, rebar and prestressing steel are used. To reduce the numerical instability with respect to the used finite element mesh size, the tension stiffening effect has been considered. For concrete, the tensile stress-strain relationship derived from tests is modified and the stress-strain curve of rebar is assumed as a simple bilinear model. The stress-strain curve of prestressing steel is applied as a multilineal curve with the first straight line up to 0.8fpu. To prove the validity of the applied material models, the behavior and strength of the PSC test specimens tested to failure have been evaluated. A reasonable agreement between the experimental results and the predictions is obtained. Parametric studies on the tension stiffening effects, the impact of prestressing losses with time, and the compressive strength of concrete have been conducted.

• 한국철도학회:학술대회논문집
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• 한국철도학회 1998년도 창립기념 춘계학술대회 논문집
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• pp.393-400
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• 1998

In this study, the crash situations and general crash analysis methods of railway rolling stocks were explained. To calculate the applied load and the maximum stress in the carbody when two aluminum railway vehicles were shunted, the finite element models for the carbody and the coupling system were made. The characteristic curve of draft gear which had a function to reduce impact force was modeled by nonlinear bar elements and the carbody was modeled by shell elements. Two shunting speeds, 5km/h and 8km/h, were considered and the results were analyzed and compared with static analysis case. Also, the aluminum railway vehicle with 60km/h was crashed against rigid wall to examine the global behavior of the carbody.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2005년도 봄학술 발표회 논문집(I)
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• pp.347-350
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• 2005

A ship collision analysis by finite element method is performed considering the effects of mass and speed of ship and material and shape of structures to analyze the dynamic characteristics by ship collision. From this analysis, collision load-time history and inelastic deformation of ship and structures are obtained. Dynamic characteristics are different from each other according to interaction. between ship and structures. It seems that there are lots of factor to have effects on the ship-structures interaction. But because little information is available on the behavior of the inelastic deformation of materials and structures during the type of dynamic impacts associated with vessel impact, assumptions based on experience and sound engineering practice should be substituted. Therefore more researches on the interaction between ship and structures are required.

• 자동차안전학회지
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• 제12권4호
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• pp.54-60
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• 2020

In a previous study, an investigation of occupant behaviors and injuries (to the head and chest) was performed during vehicle impact loading cases in order to ensure the safety of wheelchair passengers on a bus. The computational results showed overall safety tolerances of wheelchair occupants under different accident configurations. The bus crashworthiness is described as the capability of a bus to protect occupants during rollover loadings. The residual space containing occupants should be undamaged without any intrusions. However it is necessary to evaluate the residual space according to the bus occupant kinematic analysis under the rollover crash simulation. This study focuses on the evaluation of occupant behaviors during rollover loading cases in order to ensure the safety of bus passengers sitting in general seats and wheelchairs and evaluates the residual space of the bus by analyzing the bus occupant kinematics.