• 항공우주시스템공학회지
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• 제11권1호
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• pp.1-7
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• 2017

위성은 임무수행을 위하여 발사체에 탑재되어 목표하는 궤도상에 도달하게 된다. 발사체의 비행동안 위성은 사인, 랜덤, 충격과 같은 극심한 발사 진동환경에 노출되게 되며, 이에 따라 위성체 내부에 위치한 전장품 및 전장품 기판에는 각 진동요소에 의한 발사 하중이 작용하게 된다. 발사하중 작용시, 전장품 내부에 장착된 기판은 체결부를 경계로 수직방향의 굽힘 거동을 주로 일으키게 되며, 이로 인한 상대변위로 기판 위 소자의 납땜부 파괴와 도선의 단선, 기판 자체의 균열을 초래한다. 성공적인 임무 수행을 위해서, 위성의 전장품 설계는 상기 현상들에 대해 기판의 구조 건전성 및 피뢰파괴 신뢰도가 확보되어야한다. 본 논문에서는 기존에 구조해석이 기 수행되었던 다목적실용위성 3호에 탑재되는 고해상도 위성카메라용 X-band 안테나 구동장치인 APD(Antenna Pointing Driver) 전장품의 제어 보드를 대상으로 하여, 스테인버그의 식을 통해 진동 하중에 의한 허용 처짐과 최대 처짐을 도출해내고, 팔머그렌 마이너 방정식을 이용하여 수명관점에서 피로파괴 예측의 유효성을 입증하였다.

• 대한조선학회논문집
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• 제60권5호
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• pp.375-387
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• 2023

The subsea power cables are increasingly important for harvesting renewable energies as we develop offshore wind farms located at a long distance from shore. Particularly, the continuous flexural motion of inter-array dynamic power cable of floating offshore wind turbine causes tremendous fatigue damages on the cable. As the subsea power cable consists of the helical structures with various components unlike a mooring line and a steel pipe riser, the fatigue analysis of the cables should be performed using special procedures that consider stick/slip phenomenon. This phenomenon occurs between inner helically wound components when they are tensioned or compressed by environmental loads and the floater motions. In particular, Vortex-induced vibration (VIV) can be generated by currents and have significant impacts on the fatigue life of the cable. In this study, the procedure for VIV fatigue analysis of the dynamic power cable has been established. Additionally, the respective roles of programs employed and required inputs and outputs are explained in detail. Demonstrations of case studies are provided under severely sheared currents to investigate the influences on amplitude variations of dynamic power cables caused by the excitation of high mode numbers. Finally, sensitivity studies have been performed to compare dynamic cable design parameters, specifically, structural damping ratio, higher order harmonics, and lift coefficients tables. In the future, one of the fundamental assumptions to assess the VIV response will be examined in detail, namely a narrow-banded Gaussian process derived from the VIV amplitudes. Although this approach is consistent with current industry standards, the level of consistency and the potential errors between the Gaussian process and the fatigue damage generated from deterministic time-domain results are to be confirmed to verify VIV fatigue analysis procedure for slender marine structures.

• 대한조선학회논문집
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• 제30권4호
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• pp.74-82
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• 1993

본고에서는 type B 독립구형 방식 LNG 탱크의 피로균열 발생 및 진전에 대한 구조안전성 평가 기법을 연구하였다. 이는 다음과 같은 3단계의 검토과정으로 구성된다. 1) 탱크에 작용하는 파랑응력의 장기분포 평가 및 피로균열 발생수명해석 과정은 이미 제1보에서 상세히 다룬 바 있으며 2) 초기 결함이 탱크판을 관통할 수 없음을 표면균열 진전해석을 통하여 증명한다. 3) LBF(Leak Before Failure) 이론을 바탕으로 관통균열의 진전해석을 수행하여 급속 취성파괴에 대한 안전성을 검증한다.

• 한국산학기술학회논문지
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• 제21권7호
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• pp.162-167
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• 2020

본 연구에서는 국내 고정익항공기 개발의 일환으로 고정익항공기용 외부 연료탱크와 파일런에 대한 피로해석을 수행하였다. 구조해석을 통해 외부 연료탱크와 파일런의 피로해석 부위들을 선정하고, 선정된 부위들에서 단위하중에 대한 전달함수를 구축하였다. 연속 하중 프로파일에 대해서 각 프로파일 하중과 전달함수와의 내적을 통해 선정 부위에서의 응력 성분을 계산한 후, Von Mises 등가응력을 사용하여 각 프로파일의 대표응력(Representative Stress)을 계산하였다. 그리고, 구축된 대표 응력 그룹에 Rainflow Counting 기법을 사용하여 초기의 방대한 하중 프로파일로 부터 축소된 개별 프로파일과 그에 대한 진폭 및 평균값을 추출한 후, MMPDS(Metallic Materials Properties Development and Standardization)의 S-N 선도를 적용하여 수명싸이클을 계산하였다. 만약, 추출된 개별 프로파일들의 Stress Ratio가 선정된 S-N 선도의 Stress Ratio 범위를 벗어나는 경우 Modified Goodman 선도로부터 유도된 식을 사용하여 Stress Ratio가 해당 S-N 선도에서 요구하는 범위를 만족하도록 변환하는 과정을 거쳤다. 그리고, Miner's Rule에 의해 계산된 각 프로파일들의 손상값들을 더하여 선정 부위에서의 수명을 평가하였다. 최종적으로 수명평가를 위해 선정된 외부연료탱크와 파일런의 관심 부위에서 요구 수명을 모두 만족하는 것으로 평가되었다.

• Nuclear Engineering and Technology
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• 제51권4호
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• pp.1132-1141
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• 2019

Steel-concrete-steel (SCS) sandwich structures have important advantages over conventional concrete structures, however, bond-slip between the steel plate and concrete may lead to a loss of composite action, resulting in a reduction of stiffness and fatigue life of SCS sandwich structures. Due to the inaccessibility and invisibility of the interface, the interfacial performance monitoring and debonding detection using traditional measurement methods, such as relative displacement between the steel plate and core concrete, have proved challenging. In this work, two methods using piezoelectric transducers are proposed to detect the bond-slip between steel plate and core concrete during the test of the beam. The first one is acoustic emission (AE) method, which can detect the dynamic process of bond-slip. AE signals can be detected when initial micro cracks form and indicate the damage severity, types and locations. The second is electromechanical impedance (EMI) method, which can be used to evaluate the damage due to bond-slip through comparing with the reference data in static state, even if the bond-slip is invisible and suspends. In this work, the experiment is implemented to demonstrate the bond-slip monitoring using above methods. Experimental results and further analysis show the validity and unique advantage of the proposed methods.

• 한국압력기기공학회 논문집
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• 제7권1호
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• pp.35-40
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• 2011

If a plugged tube in a steam generator is broken, it may damage nearby intact tubes. To prevent this damage, it is recommended that a stabilizer is installed into the plugged tube. However, the installation cost of a stabilizer is very high. So studies are required to determine the conditions on which the installation is necessary. For this purpose static loads and dynamic loads applied on a tube should be known to estimate the residual strength and remaining fatigue and wear life of a plugged tube. Two-dimensional and three-dimensional computational fluid dynamics (CFD) analyses are performed to obtain the drag coefficient for cross flow to a tube. Using the obtained drag coefficient, the static load can be estimated and the residual strength of a plugged tube can be calculated. An inclined flow problem is also analyzed and the vertical and horizontal forces are obtained and discussed.

• Structural Engineering and Mechanics
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• 제84권6호
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• pp.823-829
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• 2022

This study considered the experimental parameters (Nano-graphene oxide reinforced polycarbonate, GFRP) under low-velocity impact load and vibration analysis. The effect of nano-graphene oxide (NGO) on a polycarbonate-based composite was studied. Two test procedures were adopted to obtain experimental results, vibration analysis. The mechanical tests were performed on damaged and non-damaged specimens to determine the damaging effect on the composite specimens. After the test was carried out, the effect of NGO was measured and damping factors were ascertained experimentally. 0. 2 wt% NGO was determined as the optimum amount that best affected the Vibration Analysis. The experiments revealed that the composite's damping properties were increased by adding the nanoparticles to 0.25 wt% and decreased slightly for the specimens with the highest nanoparticles content. Cyclic sinus loading was applied at a frequency of 3.5 Hz. This paper study the frequency effect of 3.5khz frequency damage on mechanical results. Found that high frequency will worthlessly affect the fatigue life in NGO/polycarbonate composite. In 3.5 Hz frequency, it was chosen to decrease the heat by frequency. Transmission electron microscopy (TEM) micrographs were used to investigate the distribution of NGO on the polycarbonate matrix and revealed a homogeneous mixture of nano-composites and strong bonding between NGO and the polycarbonate which increased the damping properties and decreased vibration. Finally, experimental modal analysis was conducted after the high-velocity impact damage process to investigate the defect on the NGO polycarbonate composites.

• EDISON SW 활용 경진대회 논문집
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• 제6회(2017년)
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• pp.259-269
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• 2017

Gust load is a very important load factor in designing various structures of an aircraft and judging its stability. This is because the blast effect on the aircraft in operation increases the risk of damage to the structure of the aircraft and causes a negative impact such as shortening the fatigue life by generating vibration. Particularly in the case of wing, a change in angle of attack is caused by gust load, and an additional lift acts on the wing, thereby being exposed to various excitational environments. Severe structural damage to the aircraft may occur if the natural frequencies of the aircraft wing are close to or coincident with the frequencies of the gust load applied to the wing. Recent trends of research include flight dynamics analysis considering discontinuous gusts or structural optimization of the blades under gust load. A number of studies have been conducted to interpret gust load response in consideration of irregularities in gusts. In this paper, we tried to imagine the situation of the aircraft subjected to the gust load as realistic as possible, and proposed an algorithm to track back the critical gust profile according to given aircraft characteristics from the viewpoint of preliminary engineering prediction.

• 한국도로학회논문집
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• 제11권2호
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• pp.167-174
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• 2009

본 논문에서는 아스팔트 콘크리트 포장의 표층 프로파일과 차량특성인 차량속도와 현가장치를 다르게 하여 트럭 시뮬레이션 프로그램을 통한 동적하중을 분석하였다. 다양한 포장 상태의 프로파일을 입력하여 동적하중을 분석하였으며 프로파일, 차량의 현가장치, 차량속도에 따른 동적하중 변화를 분석하였다. 포장 거칠기가 증가할수록 동적하중이 증가하였으며, 속도가 증가할 수 록 동일한 포장 거칠기 하에서 동적하중이 증가하였다. Walking beam 현가장치가 Air spring 현가장치에 비해 더 큰 동적하중을 보였다. 동적하중 공분산을 이용하여 포장파손 지수를 결정하였으며, 동적하중 공분산과 신뢰도, 아스팔트 혼합물의 파괴매개변수가 증가할 수록 포장파손지수도 증가하였다. 본 연구의 결과를 이용하여 차량속도와 표층 아스팔트 혼합물 파괴특성에 근거한 포장 평탄성 규정에 이용할 수 있으며, 아스팔트 콘크리트 포장 시공 후 포장 평탄성에 근거한 지불규정에 효과적으로 사용할 수 있다고 판단된다.

• Smart Structures and Systems
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• 제10권1호
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• pp.47-65
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• 2012

The presence of crack-like defects in mechanical and structural elements produces failures during their service life that in some cases can be catastrophic. So, the early detection of the fatigue cracks is particularly important because they grow rapidly, with a propagation velocity that increases exponentially, and may lead to long out-of-service periods, heavy damages of machines and severe economic consequences. In this work, a non-destructive method for the detection and identification of elliptical cracks in shafts based on stress wave propagation is proposed. The propagation of a stress wave in a cracked shaft has been numerically analyzed and numerical results have been used to detect and identify the crack through the genetic algorithm optimization method. The results obtained in this work allow the development of an on-line method for damage detection and identification for cracked shaft-like components using an easy and portable dynamic testing device.