• 대한기계학회논문집B
• /
• 제26권7호
• /
• pp.927-936
• /
• 2002

An experimental study has been conducted to investigate the heat/mass transfer characteristics within a film cooling hole of square cross-section for various blowing ratios and Reynolds numbers. The experiments have been performed using a naphthalene sublimation method and the flow field has been analyzed by numerical calculation using a commercial code. A duct flow enters into a film cooling hole in a cross-direction. For the film cooling hole with square cross-section, it is observed that the reattachment of separated flow and the vortices within the hole enhance considerably the heat/mass transfer around the hole entrance region. The heat/mass transfer on the leading edge side of hole exit region increases as the blowing ratios decrease because the main flow induces a secondary vortex. Heat/mass transfer patterns within the square film cooling hole are changed little with the various Reynolds numbers.

• 한국유체기계학회 논문집
• /
• 제19권2호
• /
• pp.21-26
• /
• 2016

The objective of present study is to assess the performance of the first stage compressor in a total 3-stage 5000 HP-level turbo compressor. CFD commercial code, CFX has been used to predict three-dimensional flow characteristics inside of the impeller. Shear Stress Transport (SST) model has been used to simulate turbulent flows through Reynolds-averaged Navier-Stokes (RANS) equations. Grid dependency has been also checked to get optimal grid distribution. Numerical results have been compared with the experimental test results to elucidate performance characteristics of the present compressor. In addition, flow characteristics of the impeller only have been studied for various blade configurations. Angular offset in leading edge of the blade has been selected for the optimal blade design. Performance characteristics in region of low mass flow rate and high pressure ratio between the impeller entrance and exit have been investigated for the selection of optimal blade design. Also, flow instability such as stall phenomena has been studied and anti-stall characteristics have been checked for various blade configurations in the operational window.

• 한국자동차공학회논문집
• /
• 제1권3호
• /
• pp.34-45
• /
• 1993

This study aims to analyze the mixing characteristics of hydrogen considered as a new fuel for internal combustion engines. As the physical property of helium gas is similar to that of hydrogen, helium gas was used in this study. To analyze the steady and unsteady behavior of jet, helium gas was injected into the stationary atmosphere at the normal temperature and pressure. Concentration of helium gas in the center of jet flow is in inverse proportion with axial distance from the nozzle tip. This agrees with the free jet theory of Schlichting. The relative equation for dimensionless concentration to radial/axial distance the axial distance of potential core region, the cone angle a of the jet flow and the relative equation for arriving distance of the front of jet flow to the lapse of time are obtained. But free jet theory of Schlichting in the dimensionless concentration is not in agreement with the present experimental results of the distance of the radial direction. It needs more study. When the arrival frequency of jet flow is used as a parameter, the transition area changing from unsteady flow area into steady flow area becomes gradually wider downstream, but its ratio for the whole unsteady flow area gradually decreases.

• 대한조선학회논문집
• /
• 제29권1호
• /
• pp.55-60
• /
• 1992

본 논문에서는 선형포턴셜이론을 이용하여 제한수로에 놓인 2차원 주상체에 작용하는 동유체력과 운동응답의 특성을 고찰하였다. 유체영역을, 수로입구영역 그리고 수로영역으로 구분하여 우선 각 영역에서 해를 독립적으로 구한 다음 이를 인접영역의 해와 정합시켜 완전해를 구하였다. 수로의 길이보다 대략 4배가 긴 파장의 입사파는 수로내 유동을 공진시킨다. 이때 주상체에 작용하는 부가질량은 음의 값을 갖게 되며 동유체감쇠력은 급격한 변화를 보이고 주상체의 수평운동은 최대가 됨을 밝혔다.

• 한국전자통신학회논문지
• /
• 제14권2호
• /
• pp.425-432
• /
• 2019

노즐모양이 터빈의 회전력과 축동력에 미치는 영향을 분석하기 위해, 분자 동력학 시뮬레이션을 수행하였다. 3 개의 파라메타, 노즐모양, 터빈의 회전속도 w, 분자들의 초기 속도 ($V_x,V_y$) 값들을 변화하면서, 시뮬레이션을 수행하여 터빈입구와 출구에서 분자들의 터빈 회전방향으로의 속도를 계산하였다. 이 두 영역에 걸쳐 평균 운동량을 각각 계산하고 그 차이(AMD)를 비교 분석하였다. 사용한 노즐 모양을 대상으로 AMD를 향상할 수 있는 w의 최적의 범위 도출하였으며, 터빈의 축동력 형성에 더 많이 기여할 수 있는 우수한 노즐 모양을 파악하였다.

• 한국멀티미디어학회논문지
• /
• 제13권5호
• /
• pp.651-662
• /
• 2010

본 연구는 외부환경에서 자율주행 로봇을 위해 중요한 물체를 찾기 위한 방법을 설명한다. 외부환경의 물체를 찾기 위해서 먼저 로봇은 외부환경에서 주행할 때 획득한 영상으로부터 물체를 검출하고 분할한다. 로봇은 물체의 후보를 자연물의 하늘과 나무로, 인공물의 빌딩으로 나눈다. 후보 물체를 분할하기 위해서 다중 특징을 이용한다. 다중 특징은 색상, 선분, 상황정보, 동시발생 행렬, 소실점 및 주요한 요소성분을 이용한다. 후보 특징은 물체의 특성에 맞게 혼합하여 물체를 분할한다. 이런 다중 특징은 물체에 대한 공간정보, 인간의 선험적인 지식을 이용한 물체의 기하학 정보, 공간적인 주파수 등으로 다양한 특징 추출 방법을 이용하여 물체의 영역분할의 결과를 얻는다. 물체의 분석은 분할된 영역을 이용하여 벽 영역, 창문, 정문과 같은 빌딩면의 기하학적인 속성을 찾는다. 빌딩은 소실점의 수직선분과 수평선분을 교차함으로써 그물을 얻는다. 빌딩의 벽 영역은 유사한 색상을 가지는 이웃해 있는 평행사변형의 그물을 합병해서 검출한다. 창문은 층의 수와 동일한 층에 있는 방의 수를 추정하여 빌딩의 높이와 크기를 추정한다. 실험에서 다중 특징을 이용하여 물체의 영역을 분할하고 빌딩의 기하학적인 속성을 이용하여 물체를 분석한다.

• 설비공학논문집
• /
• 제9권2호
• /
• pp.122-133
• /
• 1997

Numerical analysis using finite volume method has been carried out to examine the effect of degree of superheat of LiBr aqueous solution on heat and mass transfer occurred in absorption process. According to the result of this study, it was found that refrigerant vaper was generated at the entrance region of absorber when LiBr aqueous soltion was superheated. As the degree of superheat increases, heat transfer rate increases and vapor absorption rate decreases. The increase in averaged Nusselt and Sherwood numbers could be found as film Reynolds number increases. The larger the degree of superheat, the greater the averaged Nusselt and Sherwood numbers.

• 대한기계학회논문집
• /
• 제17권8호
• /
• pp.1921-1930
• /
• 1993

In order to evaluate the inlet pressure correctly, the full Navier-Stokes equations are solved numerically for the computational domain which covers the cavity region between pads as well as the bearing film. A nonuiform grid system is adopted to reduce the number of grid points, and the numerical solutions are obtained for a wide range of Reynolds number in laminar regime with various values of the distance between pads. The numerical results show that the inlet pressure is significantly affected by Reynolds number and the distance between pads. An expression for the loss coefficient in terms of Reynolds number and non-dimensional distance between pads is obtained on the basis of the numerical results. It is found that the inlet pressure over the whole range of numerical solutions can be fairly accurately estimated by applying the formula for the loss coefficient to the extended Bernoulli equation.

• 한국주거학회논문집
• /
• 제12권4호
• /
• pp.115-122
• /
• 2001

The purpose of this research is to analyze the survey of the residential and commercial user consciousness of 4 cases(DB, YM, TP, HG) to propose directions of development of the mixed-use apartments in Daegu. The results of the survey are as follows; 1) The residential users of DG, YM, TP and the commercial users of DG, TP, HG were not satisfied with generally present situation. 2) It showed that the development factors of the satisfaction, the reason of the move, the difficulty to operate the business, the possible use of Mixed-Use Development, the using system of the main entrance, and the reasonable residential size were the statistical significance level(p<0.05). Finally, this study proposes that 4 Cases with the diverse physical and social environment must be different with the approach, and that the reasonable residential space program, size planning for commercial unit, and choices of what kind of business should be discussed before Mixed-Use Development regarding needs of region.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2000년도 춘계 학술대회논문집
• /
• pp.120-126
• /
• 2000

An S-duct flow is subjected to an entrance flow of Mach 0.6. The duct turns $30^{\circ}$ and reverses its turn by $30^{\circ}$ followed by a straight section. Such an internal flow induces a secondary flow due to curvature effect. Goal of this paper is to show the sensitivity of outflow boundary conditions on the quality of numerical solutions as well as to show curvature effect on the flow field. The often-used Baldwin-Lomax turbulence model is shown to be less functional on the concave region when the secondary flow has its strong Influence.