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한우(韓牛)에서 면역조절세포(免疫調節細胞)의 활성(活性)에 관한 연구(硏究) : I. 말초혈액(末梢血液) 임파구(淋巴球)의 E Rosette 형성능(形成能)
유남선,김종면,송희종,채효석,강명대,이주묵,You, Nam-sun,Kim, Jong-myeon,Song, Hee-jong,Chai, Hyo-seok,Kang, Myeong-dai,Lee, Ju-mook 대한수의학회 1987 大韓獸醫學會誌 Vol.27 No.2
The erythrocytes(E) rosette forming capacity of peripheral blood lymphocytes(PBL) in Korean native cattle was determined with 2-aminoethylisothiouronium bromide hydrobromide(AET) and dextran(Dex)-treated sheep erythrocytes(SRBC). To further standardize the assay, optimum concentration of AET and/or Dex-treatment and incubation time for rosette forming cell(RFC) counts were determined. In untreated SRBC resuspended in the rosetting medium(RPMI 1640 containing 10% FCS), PBL from 7 animals formed low percentage of rosettes($7.8{\pm}6.0%$). Both AET and Dex treatment not only enhanced the rosette formation but also made it easy to enumerate rosettes by increasing numbers of SRBC attached on them. SRBC treated with 0.1M AET for 20 min or 8% Dex formed the highest percentages of rosettes, ($35.7{\pm}6.0%$ and $48.3{\pm}4.7%$, respectively) and were used in subsequent studies. With SRBC treated with 0.1M AET for 20 min and suspended in 8% Dex, the maximum RFC observed were $56.6{\pm}6.8%$ in female and $65.8{\pm}6.3%$ in male and the rates of RFC did not change significantly between 3 and 20 hr incubation time at ${4^{\circ}C}$.
등가정하중을 이용한 스프링-댐퍼 제어시스템 구조물의 최적설계에 관한 기초연구
유남선(Nam-Sun Yoo),정의진(Ui-Jin Jung),박경진(Gyung-Jin Park),김태경(Tai-Kyung Kim) 대한기계학회 2014 大韓機械學會論文集A Vol.38 No.6
본 논문은 등가정하중을 이용하여 제어시스템을 포함한 구조물의 설계를 위한 최적화 방법을 제안한다. 지난 연구는 구조물과 제어시스템 최적설계를 독립적으로 분리하여 수행하였고, 구조물과 제어시스템을 동시에 최적화하여도 제어시스템의 제어변수는 정상상태에서만 최적화하여 성능을 향상시켰다. 하지만 제어변수는 모든 시간영역에서 최적화해야 한다. 즉, 제어시스템의 해석은 과도상태에서 수행해야 한다. 본 연구에서는 새로운 등가정하중을 이용하여 제어변수를 포함하는 제어시스템 구조물의 최적설계를 위한 방법을 제시하였다. 등가정하중은 동적하중이 구조물에 작용할 때 발생하는 임의 시간에서의 변위장과 동일한 변위장을 만들어내는 정하중을 의미한다. 이렇게 계산된 등가정하중을 이용하여 설계영역에서 선형정적응답 최적설계를 진행한다. 몇 가지 예제를 통해 새로운 등가정하중을 적용한 동적응답 최적설계방법의 유용성을 확인하였다. An optimization method is proposed for the simultaneous design of structural and control systems using the equivalent static loads. In the past researches, the control parameters of such feedback gains are obtained to improve some performance in the steady-state. However, the actuators which have position and velocity feedback gains should be designed to exhibit a good performance in the time domain. In other words, the system analysis should be conducted for the transient-state in dynamic manner. In this research, a new equivalent static loads method is presented to treat the control variables as the design variables. The equivalent static loads (ESLs) set is defined as a static load set which generates the same displacement field as that from dynamic loads at a certain time. The calculated sets of ESLs are applied as multiple loading conditions in the optimization process. Several examples are solved to validate the proposed method.
박정호(Jung-Ho Park),유남선(Nam-Sun Ryu),박재범(Jae-Beom Park),정규동(Gyoo-Dong Jung) 한국추진공학회 2019 한국추진공학회지 Vol.23 No.1
Hydroxy-terminated polybutadiene (HTPB) propellants of solid rocket motors age differently under different storage temperatures. The shelf life of a solid rocket motor depends on the aging ratio of the HTPB propellant; it can be estimated through the viscoelastic properties by an aging test. This study analyzed the initial and natural aging properties during long-term storage. The initial properties were obtained from characterization and accelerated test results. The test results were obtained by analyzing the strain on cylindrical grains when a thermal load was applied.
박정호(Jung-Ho Park),유남선(Nam-Sun Ryu),박재범(Jae-Beom Park),정규동(Gyoo-Dong Jung) 한국추진공학회 2018 한국추진공학회 학술대회논문집 Vol.2018 No.5
고체 추진기관의 HTPB 추진제는 저장소에서 저장소 온도에 따라 물리적, 화학적 노화가 진행된다. 추진기관 수명은 HTPB 추진제의 노화도에 의해 결정되며, 추진기관 수명은 생산 초기에 점탄성 특성 및 노화 시험을 통해 예측된다. 본 논문에서는 생산 초기 물성 및 가속노화 시험을 통해 획득한 노화물성과 장기 저장된 자연 노화된 물성을 비교 분석 하였다. 획득된 초기 및 노화물성 결과를 적용하여 중공형 그레인의 온도 하중에 의한 변형율을 분석 하였다. HTPB propellant of Solid Rocket Motors ages by variable temperature at a storage place. Solid Rocket Motor Shelf-life depended on an aging ratio of HTPB propellant and estimated a shelf-life time through the viscoelastic property and aging test. This paper was analyzed an initial and natural aging properties during long term storaged, initial properties was obtained from characterization and accelerated test results. Cylindrical grains analyzed a strain by thermal load applying acquired test result.