• 보건의료산업학회지
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• 제10권3호
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• pp.123-133
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• 2016

Objectives : This study analyzed the effect of health-related characteristics of middle-aged and elderly people on the number of existing permanent teeth by considering each age group through the improvement of health-related characteristics. This study contributes by offering fundamental information on the prevention of dental diseases and on developing an education program that can be used by dental health businesses to improve dental health. Methods : This study used primitive data of the sixth term of the first year and the second year and selected a total of 4,393 people as the final research subject. In order to determine the factors that influence the number of existing natural teeth, confounding factors were considered, and regression analysis using general linear models was done. Results : According to the results of this research, the middle-aged and elderly groups have more existing permanent teeth in the following three cases: 1. Talking is comfortable when daily brushing frequency is 3 times or more. 2. Self-recognition of dental health condition is good. 3. Number of dental caries present in permanent teeth is low. Conclusions : For a and medical system, a dental health care system that takes into consideration the lifespans of people must be legislated and implemented.

• 한국항공우주학회지
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• 제33권11호
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• pp.95-105
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• 2005

우주시스템연구실에서는 2008년 발사 예정으로 나노위성인 HAUSAT-2를 개발하고 있다. HAUSAT-2 구조-열 모델(STM)은 구조 및 열적 설계마진을 검증하기 위하여 개발한 시스템 모델이다. HAUSAT-2의 구조-열 모델을 이용하여 인증 수준의 진동시험과 열진공/평형시험을 수행하였다. 본 논문에서는 구조-열 모델의 구조해석과 진동시험의 결과를 비교하였고 이를 통해 해석조건을 변경해 재해석을 수행하였다. 인증수준의 진동시험 결과 구조-열 모델은 구조적인 손상 없이 설계 강성 요구조건을 만족하는 것을 확인하였다. 또한 구조 조립을 통해 조립성과 인터페이스를 확인하였다.

• 한국소음진동공학회논문집
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• 제15권4호
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• pp.492-498
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• 2005

A linear motor damper based on the linear motor principle is developed to suppress structural vibration. This paper deals with the design, analysis, and manufacture of the linear motor damper. It is designed to be able to move the auxiliary mass of 1500kg, up to $\pm250mm$ stroke. The control algorithm was designed based on LQG control logic with acceleration feedback. Through performance tests, it was confirmed that the developed hybrid mass damper has reliable feasibility as a control device for structural control. In addition, the linear motor damper is more economical than both hydraulic and electric motor driving mass damper with respect to simple structure and low maintenance cost. A series of performance tests of the linear motor damper system were carried out on the full-scale steel frame structure in UNISON Corporation. Through the performance tests, it was confirmed that acceleration levels are reduced down 10dB for first mode of structure

• 한국연소학회지
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• 제20권1호
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• pp.32-42
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• 2015

The combustion instability was experimentally investigated in model gas turbine combustor with dual swirl burner. When such instability occurs, a strong coupling between pressure oscillation and unsteady heat release excites a self-sustained acoustic wave which results in a loud sound, and can even cause fatal damage to the combustor and entire system. In present study, to understand the combustion instability with a premixed mixture, the detailed periods of pressure and heat release data in unstable flame mode were investigated by various measurement methods at relatively rich condition and lean condition near flammable limits. Also, to prepare the utilization of synthetic natural gas (SNG) fuel in gas turbine system, an investigation was conducted using a simulated SNG including methane as a reference fuel to examine the effects of $H_2$ content on flame stability. These results provide that the instability due to flash-back behaviour like CIVB phenomenon occurred at rich condition, while the repetition of relighting and extinction caused the oscillation of lean condition near flammable limit. From the analysis of $H_2$ content effects, it is also confirmed that the instability frequency is proportional to the laminar burning velocity at both rich and lean condition.

• 한국태양에너지학회 논문집
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• 제35권3호
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• pp.9-16
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• 2015

In order to support various studies for assessment of onshore and offshore wind turbine system including foundations, the land-based version of 2MW PMSG direct drive wind turbine has been analyzed using HAWC2 that account for the coupled dynamics of the wind inflow, elasticity, and controls of the turbine. this work presents the steady-state response of the system and natural frequency of the first thirteen structure turbine modes as a function of wind speed. Rotor, generator speeds, pitch angle, power production, thrust force, deflections of tower and blade are compared for one case below and one case above the rated wind speed.

• Steel and Composite Structures
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• 제46권4호
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• pp.577-589
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• 2023

In this study, on-site testing was carried out to investigate the vibration performance of a cold-formed thin-walled steel floor system. Ambient vibration, walking excitation (single and double persons), and impulsive excitation (heel-drop and jumping) were considered to capture the primary vibration parameters (natural frequencies, damping ratios, and mode shapes) and vertical acceleration response. Meanwhile, to discuss the influence of cement fiberboard on structural vibration, the primary vibration parameters were compared between the systems with and without the installation of cement fiberboard. Based on the experimental analysis, the cold-formed thin-walled steel floor possesses high frequency (> 10 Hz) and damping (> 2%); the installed cement fiberboard mainly increases the mass of floor system without effectively increasing the floor stiffness and may reduce the effects of primary vibration parameters on acceleration response; and the human-structure interaction should be considered when analyzing the vibration serviceability. The comparison of the experimental results with those in the AISC Design Guide indicates that the cold-formed thin-walled steel floor exhibits acceptable vibration serviceability. A crest factor 𝛽_rp (ratio of peak to root-mean-square accelerations) is proposed to determine the root-mean-square acceleration for convenience.

• 치위생과학회지
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• 제11권4호
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• pp.353-359
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• 2011

본 연구는 치과위생사가 근무하는 병원의 미세먼지(PM-10), 포름알데히드(HCHO), 이산화탄소($CO_2$), 일산화탄소(CO), 휘발성유기화합물(VOCs) 등에 의해 오염된 실내공기가 치과위생사의 건강 및 작업능률에도 많은 영향을 끼친다는 사실을 인식하여 치과위생사를 대상으로 근무하는 병원의 냉 반방 방식 및 창문개폐를 통한 환기 횟수에 따른 실내공기질에 대한 신체자각증상 정도를 비교하고, 근무하는 병원의 실내공기질과 관련된 환경 만족에 미치는 요인을 분석하므로써 치과위생사의 건강관리를 위한 효율적인 근무환경개선방안을 제시하기 위하여 시도되었다. 조사대상자는 전국 치과병 의원에 근무하는 치과위생사로 하였으며 2010년 10월 1일 부터 2011년 1월 21일까지 자기기입식 설문조사 방식으로 582부의 설문지를 수집하여 SPSS 12.0 프로그램을 이용하여 분석하였다. 1. 냉 난방 방식별 창문 개폐를 통한 하루 환기 횟수를 비교한 결과 창문개폐를 통한 환기가 편리한 개별 냉 난방 방식에서 높은 것으로 나타났다. 2. 치과위생사는 실내공기질과 관련된 자각증상으로 인하여 불편함을 가장 많이 느끼는 시간은 오후 2시 전 후이며 불편함을 느끼기 시작한 지 1시간 경과 후인 3시 전 후에 불편함의 정도가 가장 심한 것으로 조사되었다. 3. 치과위생사의 자각증상에 따른 불편함 수준을 냉 난방 방식 및 하루 창문개폐를 통한 환기 횟수와 비교하여 분석한 결과 창문 개폐를 이용하여 자연환기가 유리한 개별 냉 난방 방식의 사무실에 근무하는 치과위생사의 수준이 낮은 것으로 나타났다. 4. 근무하는 병원의 만족에 미치는 요인을 실내공기 조건과 관련된 항목을 독립변수로 하여 중회귀 분석을 실시한 결과 "병원 공기의 냄새가 기분 좋게한다", "병원 실내 온도조건은 근무하기에 편하다", "병원의 조명은 일하기에 적당한 편이다", "병원의 환기가 잘 된다", "병원 시끄러움", "병원공기가 신선하다고 느낀다", "병원 더움" 순으로 유의하게 나타났으며 설명력은 42.9%인 것으로 나타났다.

• 동력기계공학회지
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• 제15권1호
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• pp.24-31
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• 2011

Rectangular box type structures are used in many fields of civil, mechanical and marine engineering. Especially, Most ship structures are often in contact with inner or outer fluid, like ballast, fuel and stem tanks. Fatigue damages are sometimes observed in these tanks which seem to be caused by resonance with exciting force of engine and propeller. Vibration characteristics of these thin walled tanks in contact with fluid near engine and propeller are strongly affected by added mass of containing fluid. Therefore it is essentially important to estimate the added mass effect to predict vibration of the tanks. Many authors have studied vibration of rectangular tanks containing fluid. Few research on dynamic interaction among tank walls filled with fluid are reported in the vibration of rectangular tanks recently. In case of rectangular tanks, structural coupling between adjacent panels and effect of vibration modes of multiple panels on added mass of water have to be considered. In the previous report, a numerical analysis is performed for the coupling effect between panels of a tank on added mass of containing fluid, the effect of structural constraint between panels on each vibration mode for fluid region, and mode characteristics in accordance with changing breadth of the plates by using finite element method for plates and boundary element method for fluid region. In this paper, the coupling effect between panels of a tank on added mass of containing fluid, the effect of structural constraint between panels on each vibration mode for fluid region, and mode characteristics in accordance with changing length, thickness, and boundary condition of the plates are investigated numerically and discussed.

• 한국소음진동공학회논문집
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• 제25권2호
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• pp.108-115
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• 2015

Electro-mechanical actuator installed on aircraft consists of a decelerator which magnifies the torque in order to rotate an axis connected with aircraft control surface, a control section which controls the motor assembly through receiving orders from cockpit and a motor assembly which rotates the decelerator. Electro-mechanical actuator controls aircraft altitude, position, landing, takeoff, etc. It is an important part of a aircraft. Aircraft maneuvering causes vibrations to electro-mechanical actuator. Vibrations may result in structural fatigue. For that reason, it is necessary to analyze the system structural safety. In order to analyze the system structural safety. It is needed reasonable finite element model and structural response stress closed to real value. In this paper, analytic model is derived by using the simplified finite element model, and damping ratio which is closely related to response stress is derived by using modal test. So, we developed analytic model in less than 10 % error rate, compared with modal test. Vibration response stress close to real value was estimated from analytic model modified with modal experimental damping ratio. Estimation method for damping ratio with empirical formula was suggested partly. Finally, It was proved that electro-mechanical actuator had reasonable structure margin of safety at environmental random $3{\sigma}$ stress during life cycle.

• 한국소음진동공학회논문집
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• 제22권4호
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• pp.352-357
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• 2012

The ground resonance instability of a helicopter with bearingless main rotor hub were investigated. The ground resonance instability is caused by an interaction between the blade lag motion and hub inplane motion. This instability occurs when the helicopter is on the ground and is important for soft-inplane rotors where the rotating lag mode frequency is less than the rotor rotational speed. For the analysis, the bearingless rotor was composed of blades, flexbeam, torque tube, damper, shear restrainer, and pitch links. The fuselage was modeled as a mass-damper-spring system having natural frequencies in roll and pitch motions. The rotor-fuselage coupling equations are derived in non-rotating frame to consider the rotor and fuselage equations in the same frame. The ground resonance instabilities for three cases where are without lead-lag damper and fuselage damping, with lead-lag damper and without fuselage damping, and finally with lead-lag damper and fuselage damping. There is no ground resonance instability in the only rotor-fuselage configuration with lead-lag damper and fuselage damping.