• 한국가스학회지
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• 제24권5호
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• pp.20-28
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• 2020

불산 누출사고 발생 시 피해영향범위 예측을 수계산, 영향평가 시뮬레이션, CFD 시뮬레이션을 활용하여서 예측하고 실제 환경영향보고서와 비교·분석하였다. 수계산은 누출원모델과 확산모델을 활용하여서 계산하였으며 영향평가 시뮬레이션은 우리나라 환경부에서 제공하는 KORA, 미국 환경부의 ALOHA, 상용화 프로그램 중 비교적 널리 사용 중인 PHAST를 사용하였고, CFD 시뮬레이션은 STAR-CMM+ 프로그램을 활용하였다. 사용자 입장에서 편리성, 신속성, 수용성, 경제성 등을 고려할 때 불산 누출사고 영향예측에 가장 적절하게 사용할 수 있는 프로그램은 ALOHA와 KORA 이었다. 아울러, 본 연구결과는 정부의 정책개발과 기업의 안전부서에서 피해영향범위 프레임워크를 선정하고 불필요한 규제, 불필요한 안전투자를 최적화하여 정부 또는 기업의 제한된 자원을 효율적으로 활용하는 데 도움이 될 것으로 기대된다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.763-768
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• 2011

최근 대두되고 있는 바이오가스(Biogas)를 이중 희박 예혼합 가스터빈 연소기에 적용하기 위한 연구로써, 기존 개발된 실물형 이중 희박 예혼합 연소기 버너헤드에 바이오가스 조성을 모사한 $CO_2$ 희석 연료를 사용하여, 가스터빈 연소기의 연소불안정에 미치는 영향을 연구하였다. 이중 스월이 적용된 이중화염에서 연료분배율(Pilot fuel mass fraction)에 따라 화염구조가 상이하며 이에 따라 연소장의 온도분포와 연소불안정 특성이 결정된다. 동압신호와 phase-resolved $OH^*$ 이미지를 통해 연료분배율 변화와 $CO_2$ 희석률 증가에 따른 연소불안정 크기 감소와 그 경향을 알 수 있었다. $CO_2$ 희석에 의해 열방출 섭동의 크기가 감소하고 화염속도가 감소하며 이에 따라 화염면의 팽창 즉, 체적의 증가로 인해 연소불안정이 감소되는 것을 실험을 통해 확인하였다.

• 한국위성정보통신학회논문지
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• 제11권4호
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• pp.102-106
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• 2016

스마트 폰의 대중화와 고속 무선 통신 기술의 도움으로 고품질 멀티미디어 콘텐츠가 모바일 기기에서 보편화되고 있다. 특히, Oculus Rift의 출시는 소비자 시장에서 가상현실 기술의 새로운 시대를 열고 있다. 또한 컴퓨터 게임을 보다 사실적 구동을 위한 3D 오디오 기술은 곧 차세대 모바일 기기에 적용될 것이며, 시각적인 것보다 더 광범위한 사실적 경험을 제공 할 것으로 예상된다. 따라서 이 논문에서는 가상현실 기반의 응용 프로그램에서 3D 사운드 모델링을 위한 개념, 알고리즘 및 시스템에 대하여 기술하고자 하며 특히 기하학적 음향 기술 기반의 알고리즘에 초점을 맞추었다. 이를 위하여 먼저, 사운드 전파를 모델링하기 위해 물리적 기반의 기하학적 알고리즘과 다중 채널 기술 중심으로 오디오 렌더링을 위한 중요한 설계 원칙 소개와 오디오 렌더링 파이프 라인을 씬 그래프 기반의 가상 현실 시스템 및 최신 하드웨어 구조 소개를 포함한다.

• 한국운동역학회지
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• 제16권4호
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• pp.105-113
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• 2006

The purpose of this study was to analyze the joint torque of triple segmental system in golf driver swing. For this purpose, joint torque were calculated. In order to determine the load on the lumbar region, a triple segmental system was set for wrist, left shoulder and lumbar, torque working on the lumbar region were estimated. For this study, a total of 7 professional golfers were sampled, and then, their driver swings were recorded with two high-speed digital video cameras (180 frames/sec.) to be synthesized into 3-dimensional images and coordinated. Then, Eular's equation was used to produce some kinematic data, which were used to calculate joint torque with Newton's function. All data were calculated using LabVIEW 6.1 graphic program. The results of this study can be summarized as follows; It was found that the joint torque was generated in the direction opposite the target on wrist and shoulder during down swing, while in the direction towards the target on the lumbar region. During impact and release, the torque on the wrist joint was converted from the direction opposite the target to the direction towards the target, while the torque on the lumbar region was generated vice versa. The joints on the club-arm-shoulder were generated in the opposite direction at the beginning of down swing when the torque on the thorax-pelvis began to be generated, and then, the torque on the thorax-pelvis began to lower, while that on the club-arm-shoulder began to increase. Thus, a rapid decrease of the torque on the lumbar region linked to the low trunk acted to increase moment and joint torque on the arm-club region.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 학술대회
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• pp.367-373
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• 2008

Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

• Journal of Advanced Marine Engineering and Technology
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• 제38권9호
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• pp.1163-1169
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• 2014

$CO_2$ 가스 기포 탐지 기술 개발을 위한 예비연구로 인위적으로 발생시킨 수층의 $CO_2$ 가스 기포 플룸을 다중빔음향측심기, 단일빔음향측심기 그리고 천부지층탐사기(SBP)를 이용해서 탐지 비교하였다. 인위적으로 발생시킨 기포의 상승속도는 가스 탱크에서 압축된 가스의 강제적인 누출이 영향을 미쳐 기존 자료보다 높게 나타나는 것으로 판단된다. 다중빔음향측심기는 단일빔 음향장비에 비하여 넓은 범위를 탐지할 수 있고 가스 누출 위치 및 수층에서 가스 플룸의 3차원적인 정보를 제공하고 있다. 따라서 다중빔음향측심기는 단일빔의 음향장비 보다 더 뚜렷한 가스 플룸을 탐지할 수 있으나, 상호보완적으로 동시에 운영하면 보다 효과적인 탐지기술을 확립할 수 있다. 향후, 본 연구는 특정가스의 음향학적 특징을 파악하여 정량적, 정성적 탐지 기술 향상에 기여하고자 한다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년 추계학술대회논문집
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• pp.367-373
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• 2008

Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

• Asian Pacific Journal of Cancer Prevention
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• 제15권18호
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• pp.7611-7615
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• 2014

Aims: To prepare 5-fluorouracil (5-Fu) nanoparticles with higher encapsulation efficiency and drug loading, and then investigate interaction with the SGC-7901 gastric cancer cell line. Materials and Methods: Prescription was optimized by orthogonal experiments, the encapsulation efficiency and loading capacity were tested by high-performance liquid chromatography, and inhibition of proliferation by 5-Fu nanoparticles and 5-Fu given to cells for 24, 48 and 72 hours was investigated by methyl thiazolyl tetrazolium assay (MTT). In addition, 5-Fu nanoparticles were labeled by fluorescein isothiocyanate (FITC), and absorption into cells was tested by flow cytometry. Results: The optimal conditions for preparation were concentrations of 5-Fu of 5mg/ml, of $CaCl_2$ of 60 mg/ml and of chitosan of 2 mg/ml. With a stirring speed of 1200rpm, encapsulation efficiency of 5-Fu nanoparticles was $55.4{\pm}1.10%$ and loading capacity was $4.22{\pm}0.14%$; gastric cancer cells were significantly inhibited by 5-Fu nanoparticles in a time and concentration dependent manner, and compared to 5-Fu with slower drug release, in a certain concentration range, inhibition with 5-Fu nanoparticles was stronger. 5-Fu nanoparticles were absorbed by the cells in line with the concentration. Conclusions: 5-Fu nanoparticles can inhibit growth of gastric cancer cells in vitro to a greater extent than with 5-Fu with good adsorption characteristics, supporting feasibility as a carrier.

• Journal of Electrical Engineering and Technology
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• 제10권3호
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• pp.1363-1369
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• 2015

The frequency of a power system should be maintained within the allowed limits for stable operation. When a disturbance such as generator tripping occurs in a power system, the frequency is recovered to the nominal value through the inertial, primary, and secondary responses of the operating synchronous generators (SGs). However, for a power system with high wind penetration, the system inertia will decrease significantly because wind generators (WGs) are operating decoupled from the power system. This paper proposes a dynamic droop-based inertial control for a WG. The proposed inertial control determines the dynamic droop depending on the rate of change of frequency (ROCOF). At the initial period of a disturbance, where the ROCOF is large, the droop is set to be small to release a large amount of the kinetic energy (KE) and thus the frequency nadir can be increased significantly. However, as times goes on, the ROCOF will decrease and thus the droop is set to be large to prevent over-deceleration of the rotor speed of a WG. The performance of the proposed inertial control was investigated in a model system, which includes a 200 MW wind power plant (WPP) and five SGs using an EMTP-RV simulator. The test results indicate that the proposed scheme improves the frequency nadir significantly by releasing a large amount of the KE during the initial period of a disturbance.

• 대한기계학회논문집A
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• 제40권11호
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• pp.963-970
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• 2016

본 연구는 가속페달에 반력을 생성하여 운전자의 경제운전을 유도하기 위한 에코페달의 설계와 성능 검증을 다룬다. 에코페달의 제어로직은 사전에 설정된 "허용가속도"를 바탕으로 현재 속도에서 허용되는 연료소비량을 정하고 이를 실제 연료소비량과 비교하여 에코페달의 작동을 결정하는 방식을 제안하였다. 폐달 반력은 운전자가 충분히 인지하되 불쾌감을 느끼지 않아야 하며, 차량의 정상 거동에 간섭이 없어야 한다. 스텝형과 램프형 반력 등과 같이 페달 답력이 급속하게 증가하는 형태의 반력은 반력 작동이 멈춘 직 후 운전자의 답력에 의한 급작스러운 가속 현상 때문에 적용이 어렵고, 이러한 문제가 없는 진동형 반력을 채택하였다. 진동형 반력의 주파수, 진폭, 작동시간은 운전자의 주관적 평가와 연비 향상 효과를 고려하여 결정하였다. 본 연구에서 제안된 에코페달을 차량에 장착하여 주행시험을 실시한 결과 고속도로와 시내주행에서 각각 13%와 15%의 연비향상 효과를 보여주었다.