• 한국항공우주학회지
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• 제39권5호
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• pp.424-432
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• 2011

원심압축기 임펠러의 최적화연구를 수행하기 위하여 임펠러의 형상변수와 설계변수에 관한 연구를 수행하였다. 최적화된 결과로부터 성능향상이 달성되었는지를 평가하기 위하여 기존에 실험되어진 임펠러를 선택하였으며, 이 임펠러에서 최적화를 위한 설계변수를 선정하였다. 임펠러 유로에서 허브와 쉬라우드에서의 형상은 베지어곡선으로 재설계되었다. 또한 임펠러 허브와 팁에서의 블레이드 캠버선도 베지어곡선으로 표현하였다. 각각의 형상곡선은 6-8개의 조정점으로 충분히 일치하는 곡선을 얻게 되었으며, 이 중 형상의 변화에 큰 영향을 미치는 조정점을 선택하여 8개의 설계변수로 최적화가 가능함을 보여주었다. 따라서 기존에 사용되고 있는 원심압축기 임펠러의 점 데이터를 활용하여 최적화 형상을 위한 연구가 진행될 수 있음을 보여주었다.

• International Journal of Fluid Machinery and Systems
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• 제8권4호
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• pp.274-282
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• 2015

This paper deals with the influence of leakage flow existing in SHF pump model on the analysis of internal flow behaviour inside the vane diffuser of the pump model performance using both experiments and calculations. PIV measurements have been performed at different hub to shroud planes inside one diffuser channel passage for a given speed of rotation and various flow rates. For each operating condition, the PIV measurements have been trigged with different angular impeller positions. The performances and the static pressure rise of the diffuser were also measured using a three-hole probe. The numerical simulations were carried out with Star CCM+ 9.06 code (RANS frozen and unsteady calculations). Some results were already presented at the XXth IAHR Symposium for three flowrates for RANS frozen and URANS calculations. In the present paper, comparisons between URANS calculations with and without leakages and experimental results are presented and discussed for these flow rates. The performances of the diffuser obtained by numerical calculations are compared to those obtained by the three-holes probe measurements. The comparisons show the influence of fluid leakages on global performances and a real improvement concerning the efficiency of the diffuser, the pump and the velocity distributions. These results show that leakage is an important parameter that has to be taken into account in order to make improved comparisons between numerical approaches and experiments in such a specific model set up.

• International Journal of Fluid Machinery and Systems
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• 제2권2호
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• pp.110-120
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• 2009

Generally the fluid flows within the centrifugal impeller passage as a decelerating flow with an adverse pressure gradient along the stream wise path. This flow tends to be in a state of instability with flow separation zones on the suction surface and on the front shroud. Hence several experimental attempts were earlier made to assess the efficacy of using boundary layer fences to trip the flow in the regions of separation and to make the flow align itself into stream wise direction so that the losses could be minimized and overall efficiency of the diffusion process in the fan could be increased. With the development of CFD, an extensive numerical whole field analysis of the effect of boundary layer fences in discrete regions of suspected separation points is possible. But it is found from the literature that there have been no significant attempts to use this tool to explore numerically the utility of the fences on the flow field. This paper attempts to explore the effect of boundary layer fences corresponding to various geometrical configurations on the impeller as well as on the diffuser. It is shown from the analysis that the fences located on the impellers near the trailing edge on pressure side and suction side improves the static pressure recovery across the fan. Fences provided at the radial mid-span on the pressure side of the diffuser vane and near the leading edge and trailing edge of the suction side of diffuser vanes also improve the static pressure recovery across the fan.

• 복식문화연구
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• 제11권5호
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• pp.753-766
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• 2003

The purpose of this study was to examine the cases of the family head's costume culture and to apply them to field experience education of adolescent's home economics subject. To examine the family head's costume culture, women in the family head in the Hampyeong area, Jeollanam-do were selected and interviewed. The focus of examining the family head's costume culture was on the life story of the family head, the reason to wear or possess such costume, and a motive of making. The findings of the head family's costume culture suggests that the head family of the Mos of Hampyeong had unique shroud making and custom. Also it was found that the eldest daughters-in-law of the Lees of Hampyeong have horizontally exchanged the information of the family head's costume with village women of the same family. They have initiated their costume culture directly through their daughters and it had the great influence on after-ages. The learning program for youth to experience the head family's costume culture consisted of four subjects:(l)Educating the family head's traditional living culture including etiquette training, (2)head family village walk, (3)experiencing the family head's clothes life including natural dyeing and sewing, and (4)a field trip of Hampyeong Local Life Culture Museum. For a model experience of the family head's costume life culture, three families with middle and high schoolers participated in 8- hour experience learning program. To examine the effect of learning program to experience the family head's costume culture, youth and their parents who participated in the program were asked open-ended questions, which included the content validity of experience learning, impressive experience, model experience level(difficulty), and expected effect after a model experience. As a result, their responses were found positive.

• Korean Chemical Engineering Research
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• 제46권5호
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• pp.983-987
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• 2008

IGCC 파일럿 플랜트의 집진시스템을 최적 설계하기 위하여 수치해석을 수행하였다. 서로 다른 가스 유입 방식이 집진용기 내부의 유체 유동장과 입자 거동에 미치는 영향을 분석하였다. 필터 표면에 전달되는 입자의 부하율은 분진입자가 혼합된 가스가 내부에 차단관이 설치된 집진용기의 외벽에 접하게 설치된 접선 유입구를 따라 집진용기 내로 유입되는 경우 아주 낮았으며, 입자크기가 클수록 입자부하율은 급격히 감소하였다. 이에 반하여, 가스 유동이 집진용기의 필터지지판 중앙에 수직하게 설치된 수직 유입구를 통하여 집진용기 내로 유입되는 경우, 필터 표면으로의 입자 부하율이 아주 높았으며, 입자크기 증가에 따른 입자부하율의 감소는 접선 유입 방식에 비하여 크지 않았다.

• 한국군사과학기술학회지
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• 제22권6호
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• pp.745-753
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• 2019

Recently, with the development of long-range / high-altitude guided weapon system for defense against ballistic missile, test range and firing altitude for guided weapons are increasing. Due to the increase in the test range and the intercepting altitude, it is expected to increase the range of safety area required for the firing test. Comparing to the foreign countries which have many desert or non-residence, in the domestic circumstances where the population is concentrated and distributed, it is more important to predict the falling area and to set the safety area for safely carry out the long-range / high-altitude intercept test. In this paper, we consider the following three points. The first is the booster fall trajectory modeling, the second is the shroud fall trajectory modeling, and finally, the debris dispersion modeling for the missile intercept. Especially, the AUTODYN model was used to predict debris falling area which produced in the high-speed guided missile intercepting test.

• 대한기계학회논문집B
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• 제29권4호
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• pp.485-494
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• 2005

For the extensive investigation of local heat/mass transfer on the near-tip surface of turbine blade, experiments were conducted in a low speed stationary annular cascade. The turbine test section has a single stage composed of sixteen guide vanes and blades. The chord length and the height of the tested blade are 150 mm and about 125 mm, respectively. The blade has flat tip geometry and the mean tip clearance is about $2.5{\%}$ of the blade chord. Detailed mass transfer coefficient on the blade near-tip surface was obtained using a naphthalene sublimation technique. The inlet flow Reynolds number based on chord length and incoming flow velocity is changed from $1.0{\times}10^{5}\;to\;2.3{\times}10^{5}.$ Extremely complex heat transfer characteristics are observed on the blade surface due, to complicated flow patterns, such as flow acceleration, laminarization, transition, separation bubble and tip leakage flow. Especially, the suction side surface of the blade has higher heat/mass transfer coefficients and more complex distribution than the pressure side surface, which is related to the leakage flow. For all the tested Reynolds numbers, the heat/mass transfer characteristics on the turbine blade are the similar. The overall averaged $Sh_{c}$ values are proportional to $Re_{c}^{0.5}$ on the stagnation region and the laminar flow region such as the pressure side surface. However, since the flow is fully turbulent in the near-tip region, the heat/mass transfer coefficients are proportional to $Re_{c}^{0.8}.$

• 한국압력기기공학회 논문집
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• 제20권1호
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• pp.25-31
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• 2024

The core shroud of rector vessel internals (RVI) of OPR1000 and ARP1400 is made of Type 304 stainless steel (SS) by bending and welding process that may induce high deformation and residual stress in manufacturing. This work aims to evaluate the susceptibility of stress corrosion crack (SCC) initiation of bent parts of RVI in high temperature primary water environment. For SCC initiation test, tensile specimens were fabricated from the 90 degree bent plate of Type 304 SS (DT specimen), that is an archived part of a Korean APR1400. After the SCC initiation test, the specimen surface was thoroughly examined by optical and scanning electron microscopy, and compared to the specimen fabricated from the as-received plate of Type 304 SS (AR specimen). The surface observation revealed that SCC initiated on the AR specimen surface in typical intergranular (IG) mode, while SCC on the DT specimen occurred in transgrannular mode as well as IG mode. It was also found that the size and number of SCC on the DT specimen were larger than that on the AR specimen. This was attributable to a strain-hardening during the bending process. To compare the susceptibility of SCC initiation, total crack density (TCD) was calculated from the total crack length divided by the measured area of AR and DT specimens. TCD of DT specimen was 4.6 times higher than AR specimen in average, indicating that higher possibility of degradation of bent parts of RVI for a long-term operation.

• Journal of Astronomy and Space Sciences
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• 제26권3호
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• pp.403-416
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• 2009

한국항공우주연구원에서는 기상탑재체, 해양탑재체 및 통신탑재체를 탑재한 정지궤도 위성인 통신해양기상위성을 개발하고 있다. 한국항공우주연구원에서 자체 개발한 대형 열진공 챔버를 이용하여 통신해양기상위성의 열평형 시험을 수행 할 예정이다. 열평형 시험의 주목적은 열해석 모델을 보정하고 열제어 설계를 검증하는데 있다. 통신해양기상위성의 고온 열평형 시험을 위해 남쪽과 북쪽 방열판 위에 외부 열유입량을 모사하기 위한 히팅플레이트를 장착하고, 액화질소 및 질소가스를 이용하여 히팅플레이트의 온도를 90K에서 260K 사이로 조절할 예정이다. 또한 열진공 챔버의 벽면은 심우주의 낮은 온도를 모사하기 위해 열평형 시험동안 액화질소를 이용하여 90K로 유지할 예정이다. 이 논문에서는 통신해양기상위성의 열평형 시험을 위한 열진공 챔버, 탑재체를 위한 타깃, 히팅플레이트 등 위성 모델링에 관한 내용과 열평형 시험 예측을 위한 경계조건, 부품의 작동 상태 및 온도 예측에 관해 다루고자 한다. 또한 새로이 개발한 히팅플레이트를 이용하여 열평형 시험을 수행하는 방법에 대한 타당성을 검토하고자 한다.

• Korean Chemical Engineering Research
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• 제52권3호
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• pp.279-288
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• 2014

원자력발전은 국가의 안정적인 에너지 공급원 및 저탄소 발생 에너지원으로써 기능을 해왔으나, 원자력발전에 필수적으로 발생하는 사용후핵연료 축적이라는 큰 숙제를 안고 있다. 이를 해결하기 위한 방법 중의 하나가 파이로프로세싱과 소듐냉각고속로를 연계한 사용후핵연료의 재활용이다. 용융염 전해공정을 이용하는 파이로프로세싱은 사용후핵연료에 존재하는 장 반감기 고독성 원소와 고방열 핵종을 분리하여 고준위 폐기물을 줄이면서도 고속로의 원료물질을 공급하고, 소듐냉각고속로에서는 이를 이용하여 전력을 생산한 후 다시 그 사용후핵연료를 파이로프로세싱에서 원료물질로 가공하는 개념이다. 파이로프로세싱의 전단부에 해당하는 전해환원 공정은 산화물 형태의 사용후핵연료를 금속으로 전환시켜 후속 공정인 전해정련공정에 금속을 공급하는 역할을 한다. 파이로프로세싱을 위한 전해환원 공정의 상용화를 위해서는 고용량, 고효율의 시스템 개발이 요구되므로 양극과 음극에서 공정 속도의 영향을 미치는 인자를 연구하였다.