• The Journal of Korean Society for Radiation Therapy
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• v.31 no.1
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• pp.7-15
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• 2019

Purpose: The purpose of this study is to evaluate beam delivery accuracy for small sized lung SBRT through experiment. In order to assess the accuracy, Eclipse TPS(Treatment planning system) equipped Acuros XB and radiochromic film were used for the dose distribution. Comparing calculated and measured dose distribution, evaluated the margin for PTV(Planning target volume) in lung tissue. Materials and Methods : Acquiring CT images for Rando phantom, planned virtual target volume by size(diameter 2, 3, 4, 5 cm) in right lung. All plans were normalized to the target Volume=prescribed 95 % with 6MV FFF VMAT 2 Arc. To compare with calculated and measured dose distribution, film was inserted in rando phantom and irradiated in axial direction. The indexes of evaluation are percentage difference(%Diff) for absolute dose, RMSE(Root-mean-square-error) value for relative dose, coverage ratio and average dose in PTV. Results: The maximum difference at center point was -4.65 % in diameter 2 cm size. And the RMSE value between the calculated and measured off-axis dose distribution indicated that the measured dose distribution in diameter 2 cm was different from calculated and inaccurate compare to diameter 5 cm. In addition, Distance prescribed 95 % dose($D_{95}$) in diameter 2 cm was not covered in PTV and average dose value was lowest in all sizes. Conclusion: This study demonstrated that small sized PTV was not enough covered with prescribed dose in low density lung tissue. All indexes of experimental results in diameter 2 cm were much different from other sizes. It is showed that minimized PTV is not accurate and affects the results of radiation therapy. It is considered that extended margin at small PTV in low density lung tissue for enhancing target center dose is necessary and don't need to constraint Maximum dose in optimization.

• Korean Journal of Poultry Science
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• v.19 no.2
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• pp.57-64
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• 1992

Abdominal fat pad from farmed Korean ring-necked pheasants that had scanty fat depot was characterized in terms of adipocyte size as determined by free fat cells liberated by collagenase incubation. Similar parameters was also measured in the broiler chicken with similar body weight to those of pheasants. The adipocyte from pheasants was much smaller than that of broiler chicken. The results of this study suggested that the scanty development of abdominal fat pad in the pheasants appeared to be due to a smaller size of adipocyte.

• Journal of Advanced Marine Engineering and Technology
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• v.21 no.2
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• pp.136-143
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• 1997

직경 비가 0.56인 이중동심관에 내외측모두 매끈한 벽면, 벽면 거칠기를 안측, 외측, 그리고 양측 모두의 4경우에 대한 난류 유동과 열전달특성을 실험과 이론으로 연구하였다. 시간평균속도분포, 마찰계수, 그리고 최대 속도 지점과 전단응력이 0인 지점들을 피토튜브와 X형 열선 풍속계로 측정하였다. 이중동심관내에서 4가지 경우에 따른 사각돌출형 거칠기효과가 난류 유동과 열전달에 미치는 영향을 수정난류모델을 기초로 하여 연구하였다. 직경비, 거칠기 위치, 레이놀즈수, 그리고 프란틀수 등의 여러 변수에 의해서 난류 유동과 열전달을 고찰하였다. 본 연구는 전체적 효율 측면에서 유리하게 열전달율을 향상시킬수 있는 거칠기 구조를 밝혔다.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2002.02a
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• pp.579-584
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• 2002

경남 진주시 일대에서 2001년 9월에서 12월 사이에 수확한 알타리무의 기하학적 및 물리적 특성을 측정한 결과를 요약하면 아래와 같다. 가. 동일한 지역에서 생산된 알타리무에서도 외형 및 물리적 특성의 차가 크게 나타났다. 특히 수확방법에 따라 알타리무의 외형에 손상이 생기는 것으로 나타났다. 나. 알타리무의 외형에 있어서 몸통부의 최대길이는 127.0mm, 최대직경은 59.8mm, 무청의 최대 길이는 195.0mm이다. 또한, 무청의 접합부와 몸통부의 중심부의 직경이 거의 비슷하므로 외형은 정확한 표주박형이 아닌 걸로 나타났다. 다. 몸통부에 대한 최대 압축력은 D2에서 6.50kgf로 나타났으나 평균적으로 D3에서 가장 큰 압축력을 나타내었다. 라. 알타리무의 몸통부와 무청의 접합부에 대한 최대절단력은 5.84kgf로 나타났고, 절단거리에 대한 절단력의 상관 관계는 거의 일정함을 보였다.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.174.2-174.2
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• 2013

사이클로트론에서 가속된 70 MeV 양성자 빔은 stripper에서 인출된 후 ISOL 표적에 조사하게 된다. 이 때 희귀동위원소를 생산하기 위한 ISOL 표적의 온도는 평균 $2,000^{\circ}C$ 5%로 유지하여야 한다. 사용하고자 하는 원판형태의 우라늄 표적은 직경이 45 mm 이므로 50 mm 이상의 균일한 양성자 빔이 필요하다. 본 연구에서는 stripper에서부터 ISOL 표적 까지 빔전송에 필요한 최적 조건을 연구하였다. 총 길이는 15 m 이며 두 개의 dipole을 사용하여 빔을 90도 전환시키며 3개의 4중극전자석을 사용하였다. ISOL 표적에 균일한 빔을 조사하기 위해 wobbling 방법을 활용하여 직경 50 mm 의 균일빔을 발생하고자 한다. 빔 전송 프로그램 TRANSPORT을 이용하여 stripper에서 wobbler 전까지의 빔 광학을 계산한 결과를 보고자 하고 TRANSPORT의 결과를 TURTLE 프로그램에 적용시켜 ISOL 표적에서의 균일도를 5% 미만으로 유지하는 최적조건을 발표한다.

• 한국가시화정보학회:학술대회논문집
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• 2002.11a
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• pp.27-30
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• 2002

An experimental study is performed to investigate the characteristics of near wake behind a circular cylinder with serrated fins using the constant temperature anemometer and through flow visualization. Previous report(Boo at al., 2001) shows that there are three different modes in vortex shedding behavior. This paper is focused on the identification of the physical reasons why the difference is occured in vortex shedding. The through flow velocity crossing fins decreases as increasing fin height and decreasing fin pitch mainly due to the flow resistence. Vortex shedding is affected strongly by velocity distribution around fin tube, especially by the velocity gradient. The velocity distribution at X/d=0.0 has lower gradient with increasing freestream velocity and fin height and decreasing fin pitch. Those differences in velocity gradients generate different vortex shedding mechanism.

• Transactions of the Korean Society of Mechanical Engineers
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• v.13 no.3
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• pp.538-546
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• 1989

Effect of liquid viscosity was studied experimentally on the drop size distributions of the liquid sprays from swirl atomizers. Glycerine-Water mixtures were used as test fluids for the experiments. Drop sizes of the liquid sprays were measured with the light scattering method. The concept of the standard deviation was introduced to represent the degree of uniformity of the drop size distributions. Experimental results show that the spray drops become coarser and less uniform with the liquid of higher viscosity. The effect of viscosity on the Sauter mean diameter and the standard deviation appeared to be more significant with the lower injection pressure. It was also confirmed that the Sauter mean diameter increases with the increase of the liquid viscosity and with the decrease of the injection pressure.

• Proceedings of the Korean Information Science Society Conference
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• 2010.06c
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• pp.458-462
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• 2010

본 논문은 X-선 혈관조영영상에서 기울기 정보 및 최대 빈도수를 이용한 카테터 자동 분할 방법을 제안한다. 제안방법은 세 단계로 이루어진다. 첫째, 분할하고자 하는 카테터 관심영역을 설정하고, 영상의 대조대비를 높이기 위한 밝기값 스트레칭을 수행한다. 둘째, 카테터 후보 경계점을 추출하기 위하여 카테터 방향을 고려한 경계 강조 마스크를 영상에 적용한다. 셋째, 카테터 후보 경계점에서 기울기가 크고 최대 빈도수 직경을 갖는 카테터 경계점을 추출하고 이들을 선형 보간하여 최종 카테터 경계를 분할한다. 제안 방법의 평가를 위하여 육안 평가 및 전문가가 수동 분할한 결과와 본 제안방법을 적용하여 얻은 중복 영역 비율과 평균 거리 차이를 측정한 정확성 평가를 수행하였고, 수행시간을 측정하였다. 실험결과 중복 영역 비율은 93.9%${\pm}$2.7%, 평균 거리 차이는 0.116-픽셀, 수행시간은 평균 0.011초로 측정되었다.

• Research in Plant Disease
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• v.14 no.2
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• pp.122-126
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• 2008

A stem and leaf rot disease of English ivy(Hedera helix) was found in the flower market, Jeonju, Chonbuk province, Korea in July 2007. A Phytophthora species was isolated from the diseased part of the plant. Based on the mycological properties and pathogenesis the isolate was identified as Phytophthora nicotianae. The fungus produce ovoid sporangium which was ovoid to spherical which is noncaducous, papillate and averaged $35.4{\times}25.2{\mu}m$ in dimension. Chlamydospores were abundantly produced on agar media and sized about 28.5 ${\mu}m$ in diameter. The fungus was heterothallic and A1 mating type. Oospores were measured 23.3 ${\mu}m$ in size. Optimum temperature for growth of the fungus was 25 to $30^{\circ}C$. Up to our knowledge, this is the first report demonstrating the stem rot on English ivy caused by P. nicotianae in Korea.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.11
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• pp.944-951
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• 2018

Artificial icing test and wind tunnel test can be performed to reduce the development period when a rotorcraft is required operation under icing situations. Artificial icing test of the KUH(Korean Utility Helicopter) was performed in advance to verify anti-icing and de-icing performance before natural icing test. Although high-precision sensor, the CCP(Cloud Combination Probe) is used to measure icing test condition parameters such as LWC(Liquid Water Content) and MVD(Median Volume Diameter), the measured values need to be verified in various methods due to the possibility of uncertainties which are the test atmosphere environment, sensor errors, and etc. The calculated LWC from the ice thickness cumulated on the fuselage of the KUH is compared to the measured value by CCP, and the results show the effective indirect method to check the test conditions.