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담수산 (淡水産) 이매패 (二枚貝) , 재첩의 전기영동 및 면역학적 분석
조동현,권오길,박성빈 ( Dong Hyun Cho,Oh Kil Kwon,Sung Bin Park ) 한국하천호수학회 1983 생태와 환경 Vol.16 No.3·4
Components of extrapallial fluid of Corbicula fluminea and Corrbicula sp. are comparatively examined by electrophoretic and immunochemical methods. It has been found that the proteins in extrapallial fluid of two species have some differences electrophoretically but homology immunochemicaly, In case of esterase there are some differences in activity, therefore it is suggested physiological difference in two species.
광섬유 방사선량계를 이용한 선량보강 영역에서의 심부선량 백분율과 피부 선량률 측정
조동현,장경원,유욱재,서정기,허지연,이봉수,조영호,Cho, Dong-Hyun,Jang, Kyoung-Won,Yoo, Wook-Jae,Seo, Jeong-Ki,Heo, Ji-Yeon,Lee, Bong-Soo,Cho, Young-Ho 한국광학회 2010 한국광학회지 Vol.21 No.1
본 연구에서는 고 에너지 광자선을 조사 할 때, 선량보강 영영에서의 피부 선량률을 측정을 위해 유기 섬광체와 플라스틱 광섬유를 사용한 광섬유 방사선량계를 제작하였다. 광섬유 방사선량계의 센서부에서 발생된 섬광빛은 30 m 길이의 광섬유를 통해 전달되어 광증배관과 전류계로 측정된다. 광섬유 방사선량계로 측정한 선량보강 영역에서의 피부 선량률은 이온 전리함 및 GAFCHROMIC EBT 필름의 측정 결과와 비교 및 분석 하였다. In this study, we have fabricated a fiber-optic dosimeter using an organic scintillator and a plastic optical fiber. The dosimeter measure skin dose and percentage depth dose in a build-up region for an incident high energy photon beam. The scintillating light generated in the organic sensor probe embedded in a solid water phantom is guided by 30 m plastic optical fiber to a light-measuring device such as a PMT or an electrometer. In addition, using a fiber-optic dosimeter or a GAFCHROMIC EBT film, skin dose and percentage depth dose in the build-up region are measured and compared.
담수 이매패의 진주층 형성 - ( Ⅱ. Extrapallial fluid 의 SDS 전기 영동 ) -
조동현,권오길,박성빈 ( Dong Hyun Cho,Oh Kil Kwon,Sung Bin Park ) 한국하천호수학회 1985 생태와 환경 Vol.18 No.3·4
The extrapallial fluid of two species of freshwater bivalves is studied for protein fractions. SDS-slab gel electrophoresis reveals the presence of at least 27 protein components. The insoluble matrices from the shells of Corbicula fluminea and Lanceolaria acrorhyncha are not solubilized by the method for solubilization of the avian feather keratin.
조동현,유일상,Cho, Dong Hyun,Yoo, Il Sang 한국시스템엔지니어링학회 2016 시스템엔지니어링학술지 Vol.12 No.2
Many countries concentrated on the space developments to enhance the national security and the people's quality of life. A space launch vehicle for accessing the space is a typical large complex system that is composed of the high-technology like high-performance, high-reliability, superhigh-pressure, etc. The project developing large complex system like space launcher is mostly conducted in the uncertain environment. To achieve a goal of the project, its success probability should be enhanced consistently by reducing its uncertainty during the life cycle: it's possible to reduce the project's uncertainty by performing the risk management (RM) that is a method for identifying and tracing potential risk factors in order to eliminate the risks of the project. In this paper, we introduce the risk management (RM) process applied for a Space Launch Vehicle R&D Project.
조동현,이종선,Cho, Dong-Hyun,Lee, Jong-Sun The Korean Society of Manufacturing Process Engine 2017 한국기계가공학회지 Vol.16 No.4
In the present study, we used a loop thermosyphon heat exchanger consisting of condensers with internal fins and external plate fins which are 480 mm wide, 68 mm long, and 1,000 mm high. The heat transfer pipes in the heat exchanger were 15 mm in diameter and 1,000 mm in length, and 98 heat transfer pipes were installed in the heat exchanger. According to the experimental results, as the spaces between the internal discontinuous pins decreased, the frequency of pressure drops increased and changes in temperature at the outlet of the condenser were shown to be a little smaller. Therefore, we can see that as the spaces between internal discontinuous pins decreased, the heat transfer performance increased. For the loop heat pipe heat exchanger consisting of a condenser with internal and plate fins, as the temperature of the air flowing into the condenser increased, the condensation heat transfer rate also increased, and as the condenser refrigerant inflow temperature increased, the condensation heat transfer rate increased as well.
고정된 최종시간 조건 및 추종제어 문제에 적용 가능한 수정 Φ-D 준 최적제어 알고리즘
조동현 ( Cho Dong Hyun ),이상현 ( Lee Sang Hyun ),김승필 ( Kim Seung Pil ) 공군사관학교 2017 空士論文集 Vol.68 No.1
본 논문은 시불변 시스템 뿐 아니라 고정된 최종시간이 구속조건으로 주어진 최적제어 문제와 추종제어 문제에도 적용가능 한 수정된 Φ-D 알고리즘을 제시하였다. 기존의 Φ-D 알고리즘이 대수방정식 형태의 Riccati 공식 및 Lyapunov 함수를 푸는 것이었다면, 수정된 Φ-D 알고리즘은 미분방정식 형태로 표현된 보조 상태변수를 멱급수 전개하여 푸는 방식이다. 수정된 Φ-D 알고리즘의 성능을 검증하기 위해 일반적인 형태의 고정된 시간영역 조건이 구속조건으로 주어진 비선형 최적제어 문제와 지구-화성 간 궤도전이 추종제어 문제에 수정된 Φ-D 알고리즘을 적용하여 시뮬레이션을 수행함으로써 성능을 검증하였다. 성능 검증결과 수정된 Φ-D 알고리즘 상의 제어 상수행렬인 D, T 행렬의 멱급수의 차수를 올려줌으로써 수렴한 준 최적해의 정확성을 향상시킬 수 있고, 기존의 시불변 시스템 뿐 아니라 다양한 조건(고정된 최종시간 구속조건, 추종제어 최적제어)의 최적제어 문제에 적용가능 함을 확인하였다. This paper presents a modified Φ-D algorithm that can be applied not only to the time invariant system but also to the optimal control problem given the fixed final time constraint and the regulation control problem. If the existing algorithm was to solve the Riccati formula and the Lyapunov function of the algebraic equation form, the modified algorithm is a method of solving the auxiliary state variables expressed in the form of differential equations by power series expansion. In order to verify the performance of the Φ-D modified algorithm, a nonlinear optimal control problem, which is given by a fixed final time condition as a constraint and the control problem of the Earth to Mars orbit transfer, are applied. As a result of the performance verification, it is possible to improve the accuracy of the converged suboptimal solution by raising the order of the power series. Also, it is confirmed that it is applicable not only to the existing time invariant system but also to the optimal control problem of various conditions.