• 한국산학기술학회논문지
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• 제17권11호
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• pp.363-367
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• 2016

본 연구는 마하수 2.5의 초음속 영역에서 마하수 1.0의 슬롯 분사가 있는 후향계단 형상에 대한 유동장 특성을 분석하기 위하여 초음속풍동 시험부를 설계, 제작하였다. 비행체가 고속으로 움직일 때 공동 주위의 유동은 매우 복잡하여 수치해석 결과를 검증할 초음속풍동 시험 자료가 필요하기 때문에 기존의 2차원 대칭형 노즐을 아랫면이 평판인 비대칭형 노즐로 수정하였다. 특성곡선해법을 이용한 비점성 노즐을 설계하고, 시험을 통해 얻은 경계층 두께를 노즐에 반영하여 보정한 기법을 C 언어로 프로그래밍하여 얻은 결과를 수치해석 결과와 비교하여 검증하였다. 슬롯 분사 시 지속적인 유동장 변화 분석을 위한 초음속 유지시간 확보를 위해 저장탱크의 압력 변화에 따른 PID 제어프로그램 수정으로 초음속 유동 유지시간을 약 5초에서 약 6초로 1초 정도 연장하여 제어 효율을 향상하였고, 슬롯 분사가 있는 후향계단에서의 유동장 변화를 슐리렌장치로 가시화하여 복잡한 유동장 특성을 확인하였다. 향후 슬롯 분사의 속도와 유량, 유동장의 온도를 변화하여 공동에서의 막냉각 효과 분석을 위한 장비로 사용할 계획이다.

• 자연과학논문집
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• 제15권1호
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• pp.11-34
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• 2005

전산분산시늉(computational molecular simulation)을 이용하여 생물분자와 같이 다양하고 복잡한 분자계들을 연구하는데 있어서, 그 성과는 표본추출 알고리즘의 배열공간(configuration space) 탐사능력에 의해 결정된다고 말해도 과언이 아니다. 본 연구에서는 기존의 방법들이 안고 있는 문제점들을 제거 또는 완화시킬 수 있는 유력한 방법 중 하나인 Multiensemble Sampling(MES) 방법의 실용적 속성에 대한 체계적인 연구로부터, 분자배열공간상에서 떨어져 있는 영역들을 탐사하는데 MES를 효과적으로 적용할 수 있는 체계적이면서도 일반적인 실행 방법론을 도출해 내기 위한 작업을 수행하였다. 이 작업에서는 좀 더 일반화시킨 MES의 무게함수의 꼴을 이용하여, '물속에서의 공동 형성'을 몬테카를로(MC)로 수행하였다. 여러 경우에 대해 시늉내기 매개변수들과 계산의 효율성과의 상관관계를 조사하여 그 결과로부터 효율성을 극대화할 수 있는 실행 체계를 제시할 수 있었다. 그 체계에 따라 반지름이 0에서 5.64A에 이르는 여러 크기의 공동을 갖는 계들을 한 번의 시늉으로 탐사할 수 있었다.

• 한국동물학회지
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• 제28권3호
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• pp.151-165
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• 1985

솔나방의 變態에 따른 中腸上皮의 形態的 變化를 終齡幼蟲類에서 踊化直後까지 5단계로 나누어 光學 및 電子顯微鏡을 사용하여 관찰하였다. 終齡類蟲의 中腸上皮는 圓桂狀細胞, 再生細胞 및 內分泌細胞로 구성되어 있다. 終齡幼蟲의 圓桂狀細胞에서는 核으로부터 유출되는 분비물질이 核膜에 규칙적으로 배열되어 관찰되며, 정단부에서는 lysosome이 점차 증가해 간다. 또한, 遊離綠에서는 微細絨毛사이로 팽출한 細胞質突起가 나타나는데 細胞小器官은 관찰되지 않는다. 再生細胞는 分化가 활발해짐에 따라 杯胞가 있는 杯狀細胞型으로 관찰되며, 細胞質에서는 液胞가 점차 증가한다. 踊化直前에는 Ca의 주성분으로 사료되는 물질이 동심원상으로 나타나며 杯胞는 腸內腔으로 분리된다.幼蟲類의 圓桂狀細胞에서 관찰되는 lysosome의 증가, 核物質의 細胞質로 유출, 遊離綠의 細胞質突起는 幼蟲期 中腸上皮의 退化過程을 반영하고 있다고 사료되며, 再生細胞는 杯狀細胞型으로 分化되지만 杯胞가 腸內腔으로 분리되고저 踊化期의 새로운 中腸上皮를 구성한다고 믿어진다.

• Maxillofacial Plastic and Reconstructive Surgery
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• 제34권2호
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• pp.140-147
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• 2012

Microvascular reconstruction, in the oral and maxillofacial regions, is a widely accepted as the best way to overcome the complex oral cavity defects. Many patients requiring composite reconstructions have been treated previously with radiation therapy, chemotherapy, selective and/or functional neck dissection or any of these combinations. In many cases of these patients, inadequate neck vessels for the microanastomosis of free flap are available, due to a lack of recipient vessels in the neck, poor vessel quality or vessel caliber mismatch. To achieve a tension-free anastomosis, vein grafting must be considered to span the vessel gap between the free flap pedicle and the recipient neck vessels. Although most microsurgeons believed that interpositional grafts are to be avoided due to vessel thrombosis and increased number of necessary microanastomosis, we, authors have some confidence of equivalency between reconstruction with and without interpositional saphenous vein graft. The great saphenous vein, also known as the long saphenous vein, is the large subcutaneous superficial vein of the leg and thigh. It joins with the femoral vein in the region of femoral triangle at the saphenofemoral junction, and coursed medially to lie on the anterior surface of the thigh before entering an opening in the fascia lata, called the saphenous opening. For a better understanding of the great saphenous vein graft for the interpositional vessel graft in the oral cavity reconstructions, and an avoidance of any uneventful complications during these procedures, the related surgical anatomies with their harvesting tips are summarized in this review article in the Korean language.

• Molecules and Cells
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• 제21권1호
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• pp.129-134
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• 2006

Lon, also known as protease La, belongs to a class of ATP-dependent serine protease. It plays an essential role in degradation of abnormal proteins and of certain short-lived regulatory proteins, and is thought to possess a Ser-Lys catalytic dyad. To examine the structural organization of Lon, we performed an electron microscope analysis. The averaged images of Lon with end-on orientation revealed a six-membered, ring-shaped structure with a central cavity. The side-on view showed a two-layered structure with an equal distribution of mass across the equatorial plane of the complex. Since a Lon subunit possesses two large regions containing nucleotide binding and proteolytic domains, each layer of the Lon hexamer appears to consist of the side projections of one of the major domains arranged in a ring. Lon showed a strong tendency to form hexamers in the presence of $Mg^{2+}$, but dissociated into monomers and/or dimers in its absence. Moreover, $Mg^{2+}$-dependent hexamer formation was independent of ATP. These results indicate that Lon has a hexameric ring-shaped structure with a central cavity, and that the establishment of this configuration requires $Mg^{2+}$, but not ATP.

• Bulletin of the Korean Chemical Society
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• 제22권2호
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• pp.219-227
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• 2001

The silver colloidal effects on the excited-state structure and intramolecular charge transfer (ICT) of p-N,N-dimethylaminobenzoic acid (DMABA) in aqueous cyclodextrin (CD) solutions have been investigated by UV-VIS absorption, steady-state and time-resolved fluorescence, and transient Raman spectroscopy. As the concentration of silver colloids increases, the ratio of the ICT emission to the normal emission (Ia /Ib) of DMABA in the aqueous $\alpha-CD$ solutions are greatly decreased while the Ia /Ib values in the aqueous B-CD solutions are significantly enhanced. It is also noteworthy that the ICT emission maxima are red-shifted by 15-40 nm upon addition of silver colloids, implying that DMABA encapsulated in $\alpha-CD$ or B-CD cavity is exposed to more polar environment. The transient resonance Raman spectra of DMABA in silver colloidal solutions demonstrate that DMABA in the excited-state is desorbed from silver colloidal surfaces as demonstrated by the disappearance of νs (CO2-)(1380 cm-1 ) with appearance of ν(C-OH)(1280 cm -1) band, respectively. Thus, in the aqueous B-CD solutions the carboxylic acid group of DMABA in the excited-state can be readily hydrogen-bonded with the secondary hydroxyl group of B-CD while in aqueous and $\alpha-CD$ solutions the carboxylic acid group of DMABA has the hydrogen-bonding interaction with water. Consequently, in the aqueous B-CD solutions the enhancement of the Ia /Ia value arises from the intermolecular hydrogen-bonding interaction between DMABA and the secondary hydroxyl group of B-CD as well as the lower polarity of the rim of the B-CD cavity compared to bulk water. This is also supported by the increase of the association constant for DMABA/ B-CD complex in the presence of silver colloids.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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• pp.91-93
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• 2003

A comprehensive numerical study is carried out to investigate for the understanding of the flow evolution and flame development in a supersonic combustor with normal injection of ncumally injecting hydrogen in airsupersonic flows. The formulation treats the complete conservation equations of mass, momentum, energy, and species concentration for a multi-component chemically reacting system. For the numerical simulation of supersonic combustion, multi-species Navier-Stokes equations and detailed chemistry of H2-Air is considered. It also accommodates a finite-rate chemical kinetics mechanism of hydrogen-air combustion GRI-Mech. 2.11[1], which consists of nine species and twenty-five reaction steps. Turbulence closure is achieved by means of a k-two-equation model (2). The governing equations are spatially discretized using a finite-volume approach, and temporally integrated by means of a second-order accurate implicit scheme (3-5).The supersonic combustor consists of a flat channel of 10 cm height and a fuel-injection slit of 0.1 cm width located at 10 cm downstream of the inlet. A cavity of 5 cm height and 20 cm width is installed at 15 cm downstream of the injection slit. A total of 936160 grids are used for the main-combustor flow passage, and 159161 grids for the cavity. The grids are clustered in the flow direction near the fuel injector and cavity, as well as in the vertical direction near the bottom wall. The no-slip and adiabatic conditions are assumed throughout the entire wall boundary. As a specific example, the inflow Mach number is assumed to be 3, and the temperature and pressure are 600 K and 0.1 MPa, respectively. Gaseous hydrogen at a temperature of 151.5 K is injected normal to the wall from a choked injector.A series of calculations were carried out by varying the fuel injection pressure from 0.5 to 1.5MPa. This amounts to changing the fuel mass flow rate or the overall equivalence ratio for different operating regimes. Figure 1 shows the instantaneous temperature fields in the supersonic combustor at four different conditions. The dark blue region represents the hot burned gases. At the fuel injection pressure of 0.5 MPa, the flame is stably anchored, but the flow field exhibits a high-amplitude oscillation. At the fuel injection pressure of 1.0 MPa, the Mach reflection occurs ahead of the injector. The interaction between the incoming air and the injection flow becomes much more complex, and the fuel/air mixing is strongly enhanced. The Mach reflection oscillates and results in a strong fluctuation in the combustor wall pressure. At the fuel injection pressure of 1.5MPa, the flow inside the combustor becomes nearly choked and the Mach reflection is displaced forward. The leading shock wave moves slowly toward the inlet, and eventually causes the combustor-upstart due to the thermal choking. The cavity appears to play a secondary role in driving the flow unsteadiness, in spite of its influence on the fuel/air mixing and flame evolution. Further investigation is necessary on this issue. The present study features detailed resolution of the flow and flame dynamics in the combustor, which was not typically available in most of the previous works. In particular, the oscillatory flow characteristics are captured at a scale sufficient to identify the underlying physical mechanisms. Much of the flow unsteadiness is not related to the cavity, but rather to the intrinsic unsteadiness in the flowfield, as also shown experimentally by Ben-Yakar et al. [6], The interactions between the unsteady flow and flame evolution may cause a large excursion of flow oscillation. The work appears to be the first of its kind in the numerical study of combustion oscillations in a supersonic combustor, although a similar phenomenon was previously reported experimentally. A more comprehensive discussion will be given in the final paper presented at the colloquium.

• 대한화학회지
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• 제38권5호
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• pp.339-344
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• 1994

부분적으로 $Co^{2+}$이온으로 치환한 제올라이트 A를 탈수한 후 메탄올을 흡착한 결정구조 즉 $Co_4Na_4Si_{12}Al_{12}O_{48}{\cdot}$6.5CH_3OH$ (a = 12.169(1) $\AA)$를 입방공간군 Pm$\bar3$m를 사용하여 단결정 X-선 회절법으로 해석하고 정밀화하였다. $Co_4Na_4$-A 제올라이트를 $360^{\circ}C$ 에서 $2{\times}10^{-6}$ torr하에서 2일간 진공탈수한 후 $22(1)^{\circ}C$에서 약 104 torr의 메탄올 증기로 약 1시간 동안 흡착시켜 결정을 만들었다. Full matrix최소자승법 정밀화 계산에서 I > $3\sigma(I)$인 147개의 독립반사를 사용하여 최종오차인자를 $R_1$ = 0.061, $R_2$ = 0.060까지 정밀화시켰다. 단위세포당 4개의 $Co^{2+}$ 이온과 1.5개의 $Na^+$ 이온은 6-링 산소와 결합하고 있었다. 4개의 $Co^{2+}$ 이온은 O(3)의 (111)평면에서 큰 동공쪽으로 약 0.44 $\AA$ 들어가 위치하고 1.5개의 $Na^+$ 이온은 O(3)의 (111)평면에서 소다라이트 동공 깊숙히 약 0.55 $\AA$ 들어간 자리에 위치하고 있다. 2.5개의 $Na^+$ 이온은 8-링 평면상에 위치한다. 단위세포당 약 6.5개의 메탄올 분자가 흡착되었다. 이들 메탄올 분자는 큰 동공내에 위치하고 있고, 4개의 $Co^{2+}$이온과 2.5개의 $Na^+$이온과 결합하고 있다. 4개의 메탄올의 산소는 6-링에 위치한 $Co^{2+}$이온과 결합하고 나머지 2.5개의 메탄올의 산소는 8-링에 위치한 $Na^+$이온과 결합하고 있다.

• 한국산학기술학회논문지
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• 제9권6호
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• pp.1726-1732
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• 2008

사출성형은 다양한 형태의 제품을 대량 생산할 수 있는 플라스틱 성형 공법중의 하나이다. 플라스틱 제품을 만들기 위해서는 고상의 재료를 액상으로 녹인 후 다시 고상으로 굳히는 과정을 거치는 데, 이 과정 중에 많은 문제점들이 발생을 하게 된다. 과거에는 이러한 문제를 해결하기 위해서 성형 후 금형 설계 변경 등의 시행착오적 방법을 사용하였으나, 성형과정에 대한 사출성형 CAE(Computer Aided Engineering)를 적용함으로써, 사전에 문제점을 파악하는 기술이 도입되었다. 플라스틱 제품의 큰 문제점 중 하나가 치수안정성이다. 특히 박막사출성형품은 게이트의 위치, 냉각채널과 온도에 따라서 변형량이 크게 달라진다. 본 연구에서는 현재 Stackmold방식으로 4개의 Cavity에 4개의 Hot-Runner가 설치된 금형을 통해 생산중인 DVD Tray 박막사출제품의 생산 원가 절감을 위해서 Cavity하나에 한 개의 Hot-Runner를 설계하기 위해서 CAE 해석을 통해 게이트의 위치, 냉각채널과 온도에 따라 비교하여 해석해 최적의 제품 설계를 하였다. CAE 해석에는 상업화된 CAE 프로그램인 Moldflow를 사용하였고, 수지는 PC+ABS를 사용하였다.

• Applied Microscopy
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• 제24권1호
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• pp.86-101
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• 1994

The development of synovial membrane from knee joint was studied by electron microscope in human fetuses ranging from 20mm to 260mm crown rump length (40days to 30weeks of gestational age). At 40mm fetus, developing synovial tissue was observed in homogenous interzone as a vascular mesenchyme around the periphery. The primitive joint space was appeared after the intermediate layer of the interzone in direct contact with chondrogenic layer at 60mm fetus. Differentiation of the synovial membrane coincided with clarification of the joint cauity. When dilatation of the synovial cavity occurred, the two types of synovial cells were well endowed with rough endoplasmic reticulum. At 100mm fetus, type A cells with a markedly attenuated cytoplasm were found as well as those cells which contained pinocytotic vesicles and vacuoles. By 150-200mm fetuses a majority of the intimal cells were type B. These cells were characterized by abundant rough endoplasmic reticulum and well developed Golgi complex. In contrast, A-type cell had numerous filopodia, pinocytotic vesicles lysosomes, and large vacuoles containing amorphous material. At 260mm fetus, the intimal cells were well developed and plentiful. The most marked difference between the synovial membrane of full-term fetus and adult was the large amount of collagen in the latter. During fetal period, the B-cells were most numerous cell type in the intimal cells. The B-cells were clearly distinguishable from the A-cells by their content of extensive rough endoplasmic reticulum and well developed Golgi complex.