• Parasites, Hosts and Diseases
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• 제29권1호
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• pp.21-30
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• 1991

간흡충의 충체 부위별 항원성을 알아보고자 면역조직화차적 방법을 이용하여 간흡충의 소화기관, 생식기관, 배설기관, 흡반, 표피 등의 염색강도를 비교 관찰하였다. 간흡충 실험 감염 후 2~8주 된 토끼에서 담관 내 충체를 포함하는 간 조직을 얻어 중성 포르말린 용액에 고정하고 파라핀으로 포매한 다음 4 $\mu\textrm{m}$두께로 잘라 항원으로 이용하였다. 항-간흡충 항체(1차 항체)는 실험 감염 10주 된 고양이 혈청을 희석하여 사용하였고 peroBidaseconjugated goat anti-cat IgG를 2차 항체로 하여 간접 면역효소 염색을 시행하였다. 가장 적합한 1차 항체의 희석 농도는 1 : 1,000~1 : 2,000, 2차 항체의 희석 농도는 1 : 1,000이었다. 충체의 장 상피세포, 장 내용물 및 배설낭은 1차 항체 희석 농도 1 : 1,000~1 : 2,000에서 강한 양성 반응을 보인 반면, 자궁 및 일부 자궁 내 충란, 난관선, 웅성 생식기관 등은 1차 항체 회석 농도 1 : 1,000에서 미약한 양성 반응을 나타내었다. 한편, 흡반, 표피, 표피하 세포, 충체 실질 등은 1차 항체 회석 농도 1 : 1,000에서도 음성 반응을 나타내었다. 이상의 결과를 종합하면, 간흡충 감염시 숙주의 항체 반응은 충체의 소화-분비 기관에서 유래된 이른바 분비-배설 항원에 의해 가자 강력하게 유발되는 것으로 추측된다.

• 한국전산구조공학회논문집
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• 제28권2호
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• pp.197-205
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• 2015

가스 생산용 해양플랜트 설비의 경우 폭발의 위험에 노출되어 있으며, 폭발사고는 구조물의 안전성에 치명적인 영향을 미칠 수 있다. 따라서, 이러한 폭발사고에 의한 피해를 최소화하기 위해서는, 폭발하중에 의한 구조부재의 동적응답 특성을 명확히 파악할 필요가 있다. 폭발하중의 경우 매우 짧은 시간 동안에 구조물에 가격되었다가 소멸되기 때문에 구조부재의 고유주기 및 폭발하중의 지속시간을 고려한 동적응답 평가가 필수적으로 요구된다. 일반적으로 가스 폭발하중의 경우, 부 압력단계가 전체 하중 이력에서 상당 부분 존재하며, 본 연구에서는 이러한 부 압력단계의 형상에 따라 총 하중 지속시간을 결정하는 하중 모델을 제안하였다. 방화벽은 폭발사고 시 장비 및 인명 피해를 방지하고자 FPSO 탑사이드 모듈 사이에 배치되는 구조부재이므로 폭발하중에 의한 응답이력 특성 분석이 반드시 필요하다. 때문에 무 감쇠 단 자유도 모델에 가스 폭발하중을 적용하여 변위응답 특성을 분석하였으며, 평판으로 구성된 방화벽의 FE 모델을 이용한 하중 지속시간과 구조부재들의 고유주기를 고려한 응답 특성을 분석하였다. LS-DYNA를 이용한 선형/비선형 구조해석 분석결과, 부 압력단계의 지속시간이 구조물의 동적응답에 큰 영향을 주는 것을 보였다.

• 한국균학회지
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• 제26권2호통권85호
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• pp.144-152
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• 1998

선택적 리그닌 분해능을 가지고 생물펄프공정에 사용가능한 백색부후균을 얻기 위하여 94종류의 목재부후균을 검정하였고 선발된 7개종에 대하여 활엽수와 침엽수의 부후능력을 측정하였다. 우선 백색부후균은 셀룰로오즈 분해효소, 페놀산화효소, laccase, peroxidase 등의 효소활성을 간단한 방법으로 검정하여 선발하였는데, Bavendamm test에서 양성을 나타내는 대부분의 균들은 syringaldazine을 사용한 laccase test에서도 강한 반응을 나타낸 반면, 음성반응을 나타낸 대부분의 균들은 laccase와 peroxidase test에서도 음성반응을 나타내었다. 선택적 리그닌 분해능력을 지닌 부후균을 선발하기 위하여 부후균을 은사시나무와 일본잎갈나무(낙엽송) 목재블럭에 접종하여 12주간 배양한 후에 부후된 목재의 중량감소율, 리그닌 량의 감소, 형태적 변화들을 화학분석과 주사전자현미경을 통하여 분석하는 목재부후 실험을 실시하였다. 이 실험에서 사용한 거의 모든 균주는 목재블럭의 중량감소율이 일본잎갈나무 보다 은사시나무에서 2배이상 높게 나타났으며 균을 접종하지 않은 목재블럭에서는 중량감소가 전혀 나타나지 않았다. Ceriporiopsis subvermispora와 Phanerochaete chrysosporium이 다른 균주에 비해서 침엽수와 활엽수의 리그닌을 모두 잘 분해시키는 것으로 나타났으나 분해 능력은 Ceriporiopsis subvermispora가 더욱 우수하였다. Bjerkandera adusta와 미동정된 2균주는 은사시나무에서만 상대적으로 높은 리그닌 분해능력을 나타내었다. B. adusta는 모든 세포벽 성분을 동시에 분해시켜서 2차세포벽을 얇게 만들었으나 다른 균주들은 선택적 리그닌 분해력을 나타내어 두 세포의 세포벽 사이에 위치하는 중벽에 존재하는 리그닌을 분해시켜서 세포를 분리시키는 것이 관찰되었다.

• 한국작물학회:학술대회논문집
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• 한국작물학회 2017년도 9th Asian Crop Science Association conference
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• pp.93-93
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• 2017

To develop rice cultivars with increased biomass and grain yield, superior lodging resistance is an essential trait. The new breeding approach can be adopted for the improvement of stem lodging resistance by enhancing culm strength. The resistance to breaking type lodging is attributed to bending moment of basal culm (M), which is composed of the section modulus (SM) and bending stress (BS). The resistance to the bending type lodging is attributed to flexural rigidity (FR) of stem, which is composed of the secondary moment of inertia (SMI) and Young's modulus (YM). Starch and cell wall components such as cellulose, hemicellulose and lignin also play a significant role in physical strength of culm, and thus affect lodging. Leaf Star has a superior lodging resistance due to its thick and stiff culm because of its high M and FR compared with Koshihikari. Furthermore, Leaf Star contains high densities of hemicellulose, cellulose and low lignin density in culm compared with Koshihikari. In this study, we performed QTL analysis for these traits associated with culm strength, using 94 recombinant inbred lines (RILs, $F_8$), derived from a cross between Leaf Star and Koshihikari. The SM in the RILs showed a continuous distribution. QTLs for SM were detected on chrs.2, 3 and 10. Leaf Star alleles increased SM on chrs. 2 and 3, but Koshihikari allele increased on chr.10. These QTLs overlapped with those QTLs identified using backcrossed inbred line derived from a cross between Chugoku 117 and Koshihikari, the parents of Leaf Star. The FR in Leaf Star was higher than that in Koshihikari due to the larger SMI and YM. 3 QTLs for SMI were detected on chrs.2, 3 and 10. Leaf Star alleles increased SMI on chrs.2 and 3, and Koshihikari alleles increased on chr.10. One QTL on chr.3 and two QTLs on chr.5 for hollocelulose content were detected with Leaf Star alleles contribution. Moreover, two QTLs were detected for hemicellulose density on chrs.3 and 5. Leaf Star allele increased hemicellulose density on chr.5, and Koshihikari allele increased on chr.3. Furthermore, two QTLs for cellulose density were detected on chr.5, and one QTL on chr.2. For starch content, one QTL on chr.3 and two QTLs on chr.5 with Leaf Star alleles contribution were detected. TULK-6 carrying a chromosome segment of Leaf Star on chr.5 in the Koshihikari genetic background showed higher densities of starch and hemicellulose than those in Koshihikari. These results suggest that the detected QTLs for culm strength could be utilized for the improvement of lodging resistance in rice by marker-assisted selection.

• 한국작물학회:학술대회논문집
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• 한국작물학회 2017년도 9th Asian Crop Science Association conference
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• pp.133-133
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• 2017

Lodging is one of the important constraints in rice production. The lodging destroys the canopy structure, and sharply reduces the capacity of photosynthetic rate and dry matter production. In cereal crops, stem lodging can be classified into two types: stem breaking type and stem bending type. To improve stem lodging resistance, it is important to reveal strong culm traits of superior lodging resistant varieties. There are large varietal differences in parameters associated with the bending moment at breaking (M) and flexural rigidity (FR). The indica variety Takanari possesses large M due to its large section modulus (SM) despite of its small bending stress (BS), while Takanari also has large FR due to its large secondary moment of inertia (SMI) and Young's modulus (YM). To identify quantitative trait loci (QTLs) and the corresponding genes associated with the parameters for M ($=SM{\times}BS$) and FR ($=SM{\times}YM$) should enable to develop lodging resistant varieties, efficiently. In order to identify QTLs for cell wall materials such as cellulose, hemicellulose and lignin associated with BS and YM, a set of Chromosome Segment of Substitution Lines (CSSLs) consisted of 37 lines with chromosome segments of Koshihikari in the genetic background of Takanari were used. Takanari had large M and small BS as compared with Koshihikari. The QTLs for BS were estimated on chromosomes 3, 5, 6, 8, 9, 10, 11 and 12. Koshihikari alleles increased BS in these QTLs. Takanari had a large FR due to its large SMI and YM as compared with Koshihikari. The YM was increased by substitution of the Koshihikari chromosomal segments on chromosomes 2, 10 and 11. Other QTLs estimated on chromosomes 7 and 12 that Koshihikari alleles contributed to the decrease of YM. For lignin, only one major QTL for lignin density was detected on chromosome 11. Hollocellulose densities were increased by the substitution of Koshihikari segments on chromosomes 5 and 11. On the other hand, these were decreased on chromosomes 1 and 3 by substitution of Koshihikari segments. QTLs for cellulose density were estimated on chromosomes 1, 3 and 5 by substitution of Koshihikari segments. For hemicellulose, QTL on chromosome 3 showed that hemicellulose density decreased by the substitution of Koshihikari segment. However, hemicellulose densities on chromosomes 5, 8 and 11 showed the opposite effects. The QTLs for hemicellulose, cellulose, and hollocelulose densities identified on chromosome 5 overlapped with that for bending stress, indicating the positive effect of Koshihikari segment on increasing bending stress. These results suggest that some QTLs for the densities of cell wall materials contribute to increasing bending stress and Young's modulus, and could be utilized to improve the lodging resistance for both types of breaking and bending in rice varieties.

• 한국가시화정보학회:학술대회논문집
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• 한국가시화정보학회 2002년도 추계학술대회 논문집
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• pp.1-6
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• 2002

How is the flow in a rotating impeller. About 35 years have passed since one experimentalist rotating with the impeller. of a huge centrifugal blower made the flow measurements using a hot-wire anemometer (Fowler 1968). Optical measurement methods have great advantages over the intrusive methods especially for the flow measurement in a rotating impeller. One is the optical flow visualization (FV) technique (Senoo, et al., 1968) and the other is the application of laser velocimetry (LV) (Hah and Krain, 1990). Particle image velocimetries (PIVs) combine major features of both FV and LV, and are very attractive due to the feasibility of simultaneous and multi-points measurements (Hayami and Aramaki, 1999). A high-pressure-ratio transonic centrifugal compressor with a low-solidity cascade diffuser was tested in a closed loop with HFC134a gas at 18,000rpm (Hayami, 2000). Two kinds of measurement techniques by image processing were applied to visualize a flow in the compressor. One is a velocity field measurement at the inducer of the impeller using a PIV and the other is a pressure field measurement on the side wall of the cascade diffuser using a pressure sensitive paint (PSP) measurement technique. The PIV was successfully applied for visualization of an unsteady behavior of a shock wave based on the instantaneous velocity field measurement (Hayami, et al., 2002b) as well as a phase-averaged velocity vector field with a shock wave over one blade pitch (Hayami, et al., 2002a. b). A violent change in pressure was successfully visualized using a PSP measurement during a surge condition even though there are still some problems to be overcome (Hayami, et al., 2002c). Both PIV and PSP results are discussed in comparison with those of laser-2-focus (L2F) velocimetry and those of semiconductor pressure sensors. Experimental fluid dynamics (EFDs) are still growing up more and more both in hardware and in software. On the other hand, computational fluid dynamics (CFDs) are very attractive to understand the details of flow. A secondary flow on the side wall of the cascade diffuser was visualized based either steady or unsteady CFD calculations (Bonaiuti, et al.,2002). EFD and CFD methods will be combined to a hybrid method being complementary to each other. Measurement techniques by image processing as well as CFD calculations give a huge amount of data. Then, data mining technique will become more important to understand the flow mechanism both for EFD and CFD.

• 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.

• 대한기계학회논문집B
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• 제34권4호
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• pp.437-442
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• 2010

고온, 고압의 유체가 흐르는 탄소강 배관에서는 유동가속부식으로 인한 배관감육 현상이 발생할 수 있다. 화력 및 원자력발전소에서 유동가속부식으로 인한 배관 손상시 고비용의 보수와 발전 정지를 유발할 뿐 아니라 발전소 신뢰도 및 안전성에 영향을 미칠 수도 있다. CHECWORKS 프로그램은 국내 발전소에서 유동가속부식에 의한 배관 손상을 예방하기 위하여 배관 두께검사 데이터를 평가하고 검사 계획을 수립하는데 이용되어 왔다. 그러나 상기 프로그램은 원전 2차측 배관 모두를 데이터베이스화한 후에 배관라인 그룹별로 유동가속부식 손상을 예측하기 때문에 국부적으로 감육에 민감한 부위를 찾는데 어려움이 있다. 본 논문에서는 CHECWORKS 프로그램을 이용하여 해석을 수행하고 수치해석을 통하여 검증할 수 있는 방법론을 기술하였다. 또한 국내 원전 2개의 배관 라인그룹에 대하여 CHECWORKS 프로그램을 이용한 유동가속부식 민감 부위를 FLUENT를 이용한 수치해석 결과와 비교하였다.

• Advances in pediatric surgery
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• 제4권2호
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• pp.156-162
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• 1998

저자들은 1983년 1월부터 1998년 1월까지 총담관낭 환아 28례 중 4례(14.2 %)에서 자연적으로 발생한 총담관낭 천공에의한 담즙성 복막염을 경험하였고 이 중 3례에서 일차적인 낭종 절제와 간관공장 문합술을 시행하였으며 이 모든 예에서 합병증 없이 회복되었기에 문헌 고찰과 함께 보고하는 바이다. 총담관낭 천공에의한 답즙성 복막염치료는 일차적 낭종 절제와 간관 공장 문합술이 안전하고 효과적인 방법이라고 생각된다.

• 한국산림과학회지
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• 제46권1호
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• pp.44-52
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• 1980

이 연구(硏究)의 목적(目的)은 우리나라의 주요(主要)한 수종(樹種)인 잣나무에 대(對)하여 fibril 경사각(傾斜角)의 변이(變異)을 알아 보기 위한 것이다. 1937년(年)에 I. W. Bailey 씨(氏)는 옥도(沃度)의 침상결정(針狀結晶)을 통하여 가도관이차막중층(假導管二次膜中層)이 fibril 경각측정(傾角測定)의 가능성(可能性)을 발표(發表)하였다. 그래서 필자(筆者)는 일본(日本)의 소림미일씨(小林彌一氏)의 간편법(簡便法)을 이용(利用)하여 이 연구(硏究)를 시도(試圖)하였는데 요약(要約)하면 다음과 같다. 1. Fibril 각도(角度)는 추재(秋材)보다는 춘재(春材)에서 더 크게 나타나 있다. 2. Fibril 경각(傾角)은 수피(樹皮)쪽 보다는 수(髓)쪽이 더 크게 나타나 있다. 3. 수(髓)에서 수피(樹皮)쪽으로 이행(移行)함에 따라 춘(春) 추재(秋材)의 차이(差異)는 수(髓)에 가까운 쪽에서 가장 크게 나타나 있다.