• Journal of Advanced Marine Engineering and Technology
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• 제25권4호
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• pp.825-832
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• 2001

This study was experimentally performed to investigate freezing behavior of sea water along horizontal cooled a circular tube with bubbly flow. The experiments were carried out for a variety of parameter, such as sea water velocity, air-bubble flow rate, and cooled-tube temperature. The shape of freezing layer, freezing rate and salinity of frozen layer were observed and measured. And the flow patterns around cooled tube were visualized using the PIV to analyze the relationship between the flow structure and the freezing characteristics. It was found that the experimental parameters gave a great influence on the freezing rate and the salinity of the frozen layer.

• 한국유체기계학회 논문집
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• 제10권1호
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• pp.26-33
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• 2007

Four design candidates for a partial admission turbine have been chosen from a preliminary design process. Their performance were estimated through the 3-D numerical analyses using a frozen rotor method. In order to select the optimum design, each flow analysis result was compared with others. Flow characteristics in the passages and some types of losses induced by shocks and wakes were found from calculation results. Based on these calculations, a new rotor blade was redesigned and compared with previous one through flow analysis.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2001년도 제22회 KOSCI SYMPOSIUM 논문집
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• pp.90-98
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• 2001

Characteristics of high temperature rocket nozzle flow is discussed along with the aspects of computational analysis. Three methods of nozzle flow analysis, frozen-equilibrium, shifting-equilibrium and non-equilibrium approaches, were discussed, those were coupled with the methods of computational fluid dynamics code. A chemical equilibrium code developed for the analysis of general hydrocarbon fuel was coupled with three approaches of nozzle flow analysis. The approaches were used for the performance prediction of KSR-III Rocket, and compared with the theoretical results from NASA CEA (Chemical Equilibrium with Applications) code.

• 항공우주시스템공학회지
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• 제1권1호
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• pp.67-72
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• 2007

In this paper, numerical results for 3-D supersonic turbine flow have been firstly compared with the experimental results to verify results computed by $Fine^{TM}/Turbo$. It was found that $Fine^{TM}/Turbo$ can accurately predict flow characteristics within supersonic turbine. Next, an grid system for 3D turbine flow was optimized selected through grid independency test. Finally, the effect of axial gap between rotor and nozzle and chamfer angle of blade edge on the flow characteristics within 3-D supersonic turbine was analyzed with Frozen Rotor method.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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• pp.445-451
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• 2004

Four design candidates for a 1.4MW class partial admission turbine have been chosen from a Preliminary design process. Their performance were estimated through the 3-D numerical analyses using a frozen rotor method. In order to select the optimum design, each flow analysis result was compared with others. Flow characteristics in the passages and some types of losses induced by shocks and wakes were found from calculation results. Based on these calculations, a new rotor blade was redesigned and compared with previous one through flow analysis.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제29회 추계학술대회논문집
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• pp.105-109
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• 2007

로켓 노즐 유동해석에는, 전산 유체 역학 코드와 결합된 동결 유동 해석, 화학 평형 해석, 화학 비평형 해석이 사용되어진다. 고온 로켓 엔진 노즐의 설계에서, 동결 유동 해법과 동일한 수치적 특징을 가지는 화학평형 해석은 노즐의 열역학적 최대 성능을 예측하는 효율적인 설계 도구가 될 수 있다. 본 연구에서는 30톤급 KARI 액체 로켓 엔진 노즐에 대하여 동결유동 해석 및 화학평형 유동 해석을 수행하였다. 유동 해석 결과에 기초한 30톤급 KARI 액체 로켓 엔진 성능 평가는 노즐에서의 열화학적 특성에 대한 이해와 노즐의 성능을 제공할 것이다.

• Reproductive and Developmental Biology
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• 제28권3호
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• pp.167-172
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• 2004

Flow cytometry를 이용하여 개 정자의 생존율 평가를 수행하고자 2-4세의 수캐 5두가 이용되었고, 분석을 위해 PI염색을 실시하였다. Flow cytometry를 이용한 개 신선 정액의 생존율 평가는 생존 정자와 죽은 정자의 비율을 1:0, 1:1, 1:3으로 조성하여 이를 flow cytometry로 평가하고 광학현미경검사, CFDA/PI 염색검사, HOS test에 의한 생존율과 비교하여 flow cytometry와의 상관관계를 알아보았다. 또한 개 정액을 동결하여 응해 후의 개 정자의 생존율 평가에도 동일한 방법으로 상관관계를 조사하였다. 신선 정액에서 생존 정자와 죽은 정자의 비율이 1:0, 1:1, 1:3 모든 경우에서 flow cytometry를 이용한 생존율은 HOS test에 의한 생존율과 높은 상관관계를 나타내었다 (p<0.01). 신선 정액에서 생존 정자와 죽은 정자의 비율이 1:0과 1:3일 때 광학현미경적 검사에 의한 생존율은 flow cytometry 분석에 의한 생존율과 유의 적인 상관관계를 나타내었으나 (p<0.05), 1:1 비율의 경우 상관관계를 보이지 않았다. 신선 정액에 생존 정자와 죽은 정자의 비율이 1:0과 1:1일 때 CFDA/PI 염색 검사에 의한 생존율은 flow cytometry분석에 의한 생존율과 높은 상관관계를 보였으며(p<0.01), 1:3 비율에서는 유의적인 상관관계를 보였다 (p<0.05). 동결 및 응해 후의 개 정자의 생존율 평가에서 HOS test 결과는 flow cytometry분석에 의한 생존율과 높은 상관관계를 보였으며 (p<0.01), 광학현미경적 검사를 통한 생존율은 유의적인 상관관계를 보였으나 (p<0.05), CFDA/PI 염색 검사결과는 상관관계를 보이지 않았다. 이상의 결과 flow cytometry는 신선정액 및 동결 융해 후 개 정자에 대한 생존율 검사에 정확한 평가 방법 인 것으로 판단되었다.

• 동력기계공학회지
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• 제15권4호
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• pp.42-47
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• 2011

The purpose of this study is to investigate the best melting condition with various winding number of a heating pipe, supplying quantity of engine coolant and coolant temperature at the inlet of the heating pipe. Also, it is to suggest getting method of an appropriate quantity of the agent for the urea-SCR system within 10 minutes. For this matter, this study identifies the temperature distribution of inside of urea-tank while it is frozen at the low temperature condition, and suggests the best melting condition of the frozen urea within 10 minutes. From the results, it was found that 2L of melted urea was obtained by the coolant flow rate of 200L/hr at $70^{\circ}C$ for 10 minutes from the start of engine operating.

• 항공우주기술
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• 제4권2호
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• pp.153-162
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• 2005

초기 설계과정에서 4가지 1.4MW급 터보펌프용 터빈설계안을 도출한 후 각각의 설계안에 대하여 프로즌 로터기법을 적용한 3차원 유동해석을 수행하였다. 이 결과를 통하여 각각의 설계안간의 성능을 비교하고 가장 성능이 우수한 설계안을 선정하였다. 계산결과의 분석을 통하여 유로에서의 유동특성과 충격파와 후류에 의해 발생되는 손실을 파악하였으며 이 분석 결과를 바탕으로 보다 우수한 성능을 보일 것으로 예측되는 설계안을 도출한 후 이에 대한 3차원 유동해석을 수행하여 결과를 분석하였다.

• Journal of Mechanical Science and Technology
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• 제15권1호
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• pp.125-138
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• 2001

An efficient correction storage scheme on a structured grid is applied to a sequence of approximate Jacobian systems arising at each time step from a linearization of the discrete nonlenear system of equations, obtained by the implicit time discretization of the conservation laws for unsteady fluid flows. The contribution of freezing the Jacobian matrix to computing costs is investigated within the correction storage scheme. The performance of the procedure is exhibited by measuring CPU time required to obtain a fully developed laminar vortex shedding flow past a circular cylinder, and is compared with that of a collective iterative method on a single grid. In addition, some computed results of the flow are presented in terms of some functionals along with measured data. The computational test shows that the computing costs may be saved in favor of the correction storage scheme with the frozen Jacobian matrix, to a great extent.