• 한국가시화정보학회지
• /
• 제17권3호
• /
• pp.12-18
• /
• 2019

Direct numerical simulation of a fully developed turbulent plane Couette-Poiseuille flow with a two-dimensional (2-D) rod-roughened wall is performed to investigate the impacts of the surface roughness. It is shown that the logarithmic region in the mean velocity profile over the rough wall Couette-Poiseuille flow is significantly shortened by the surface roughness compared to that over a turbulent Couette-Poiseuille flow with smooth wall. The Reynolds shear stress over the rough wall Couette-Poiseuille flow is decreased compared to that for a smooth case in the outer layer. These results are attributed to weakened turbulence activity or roll-cell mode over the rough wall Couette-Poiseuille flow near the channel centerline due to suppressed development of u'-structure on the top wall, as documented through spanwise energy spectra of the streamwise velocity fluctuations. Inspection of congregation motion near the bottom wall and time evolution of u'-structure reveal weakened co-supporting cycle for the rough wall case.

• 한국자동차공학회논문집
• /
• 제6권4호
• /
• pp.101-107
• /
• 1998

A three-dimensional multi-phase flow is simulated around a smooth tire. This simulation is conducted by solving Navier-Stokes equation with a k-$\varepsilon$ turbulent model. The numerical calculations are carried out by modeling a multi-phase free surface flow mixed with air and water at the inlet. The numerical solutions show an intuitively resonable behavior of water around a moving tire. The calculated pressure around the tire surface along the moving direction is presented. The moving velocities of the tire are chosen to be 30, 40, 60, and 70 km/h. The numerically simulated pressures around the tire are compared with existing experimental data. The comparison shows a new possible tool of analyzing a hydroplaning phenomenon for an automobile tire by means of a computational fluid dynamics.

• 대한기계학회논문집
• /
• 제19권1호
• /
• pp.219-230
• /
• 1995

The flow characteristics of a two-dimensional offset jet issuing parallel to a rough wall is experimentally investigated by using a split film probe with the modified Stock's calibration method. The mean velocity and turbulent stresses profiles in the up and down-stream locations of the wall-attachment regions are measured and compared with those of the smooth wall attaching offset jet cases. It is found that the wall-attachment region on the rough wall is wider than on the smooth wall for the same offset height and the jet speed. The position of the maximum velocity point is farther away from the wall than that for the smooth wall case because of the thick wall boundary layer established by the surface roughness. It is concluded that the roughness of the wall accelerates the relaxation process to a redeveloped plane wall jet and produces a quite different turbulent diffusion behavior especially near the wall from comparing with the smooth plane wall jet turbulence.

• 대한기계학회논문집
• /
• 제15권6호
• /
• pp.2083-2099
• /
• 1991

본 연구에서는 다른 실험 조건은 일정하게 유지하면서 아래 벽면의 표면조도 를 체계적으로 변화시켜 표면조도가 후향계단 뒤의 재부착 흐름 및 재발달경계층에 미 치는 영향을 조사하고자 하며 구체적인 내응은 다음과 같다. (1) 표면조도가 재부착 길이와 재발달경계층에 미치는 영향의 조사. (2) 표면조도가 평균속도와 난류량 분포 에 미치는 영향의 조사. (3) 여러 종류 표면조도 변화에 따른 재부착길이와 재발달 경 계층 회복에 미치는 영향과 결과의 상호 비교.

• 한국가시화정보학회지
• /
• 제12권3호
• /
• pp.15-20
• /
• 2014

Direct numerical simulation (DNS) dataset of a turbulent boundary layer (TBL) with a step change from smooth to rough surface is analyzed to examine spatially developing flow characteristics. The roughness elements are periodically arranged two-dimensional (2-D) spanwise rods with a streamwise pitch of ${\lambda}=8k$ ($=12{\theta}_{in}$), and the roughness height is $k=15{\theta}_{in}$, where ${\theta}_{in}$ is the inlet momentum thickness. The step change is introduced $80{\theta}_{in}$ downstream from the inlet. For the first time, full images from the DNS data with the step change from the smooth to rough walls is present to get some idea of the geometry of turbulent coherent structures over rough wall, especially focusing on their existence and partial dynamics over the rough wall. The results show predominance of hairpin vortices over the rough wall and their spanwise scale growth mechanism by merging.

• 한국수자원학회논문집
• /
• 제39권9호
• /
• pp.737-744
• /
• 2006

난류의 내부 영역의 유속은 단순한 공식으로 표현하기 매우 어려운 형태를 가지고 있다. 이 속도 분포를 기술하는 여러 가지 공식들이 제안된 바 있지만, 모든 공식들은 많은 항들을 가지거나 적분형 또는 음함수꼴을 가지고 있다. 이것은 이 식들이 적용하기 힘들거나, 매개 변수들을 추정하기 어렵다는 것을 의미한다. 이 연구에서는 매끄러운 바닥 위를 흐르는 난류 내부 영역의 유속 분포를 표현할 수 있는 간단한 형태의 새로운 공식을 제안하였다. 이 공식은 전통적인 대수 법칙에 감쇄 함수를 곱한 형태이다. 단 하나의 추가적인 매개 변수를 도입하여, 전체 내부 영역의 유속 분포를 적절하게 표현할 수 있었다. 이 공식은 벽법칙이 성립하는 바닥 근처의 유속과 대수 법칙이 성립되는 중복 영역의 유속 분포까지를 적절하게 나타낼 수 있다. 또한, 추가된 매개 변수인 감쇄 계수는 쉽게 추정할 수 있다. 이 변수는 Reynolds 수의 변화에 민감하지 않으며, 공식에 의하여 계산된 유속 분포도 또한 이 매개 변수의 변화에 대해서 민감하지 않다.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2007년도 춘계학술대회B
• /
• pp.2660-2665
• /
• 2007

Turbulent boundary-layer over a micro-riblet film(MRF) was investigated experimentally. The MRF has sharp V-shaped micro scale grooves of $300{\mu}m$ in width and $176.8{\mu}m$ in height. Particle image velocimetry(PIV) system was employed to measure velocity fields of flow over the MRF coated plate. Flow over a smooth plate was also measured for comparison. The PIV measurements were taken in the streamwise wall-normal planes at Re$\theta$= 985 and 2342. Vortex structures of the flow were analyzed by extracting the swirling strength as an unambiguous vortex-identification criterion. As a result the number of spanwise vortices with clockwise(negative) rotation decreases rapidly in the near-wall region(y<0.2h), but decreases slowly in the outer region(0.2h

• 물과 미래
• /
• 제28권2호
• /
• pp.155-168
• /
• 1995

본고는 개수로 마찰계수를 산정하거나 단면평균유속을 구하는 전통적인 방법의 경험식을 논의하였으며, 새로운 형태의 산정식을 제시하였다. 기존 경험식중 형태가 가능한 것은 차원의 일치를 기하기 위하여 수정하였으며, 등가조고를 도입하여 새로운 형태의 경험식을 제안하였다. 개수로에서의 마찰계수 분포도 원형판에서의 완난류 마찰계수 분포와 유사함을 고려하여 대부분의 관측자료는 완난류 구간에 드는 것으로 판단하였으며, 원형관 완난류 마찰계수 산정식을 수정하여 사각형 개수로 완난류 마찰계수 산정식을 개발하였다. 또한 차원의 일치를 이룬 새로운 형태의 경험식들을 포함하여 이들 산정식을 Bazin의 실험자료에 적용하여 비교 검토하였다.

• 대한기계학회논문집
• /
• 제19권7호
• /
• pp.1749-1757
• /
• 1995

The structure of turbulence of fully developed flow through three concentric annuli with both rough inner and outer walls was investigated experimentally for Reynolds number range Re=15000-93000. Turbulence intensities were measured in three (u, v, w) directions, and turbulence shear stresses in annuli of radius ratios .alpha.= 0.26, 0.4 and 0.56, respectively. The result showed that the structure of turbulence for these asymmetric flows was not the same as that for the annulus with smooth walls. The velocity fluctuations of all three components (u, v, and w-directions) showed little discernible variation with Reynolds numbers, but became apparent with the influence of radius ratio (.alpha.) The experimental results for an annulus with the roughened outer wall and a smooth annulus were shown in the figures as a reference. The eddy diffusivities and friction factors were also presented and discussed.

• 대한조선학회지
• /
• 제21권2호
• /
• pp.9-17
• /
• 1984

Laminar and turbulent boundary layers on a rotating sector and a helical blade are calculated by differential method. The estimation of three dimensional viscous flows provide quite useful informations for the design of propellers and turbo-machinery. A general method of calculation is presented in this paper. Calculated laminar boundary layer on a sector shows smooth development of flows from Blasius' solution at the leading edge to von Karman's solution of a rotating disk at the down-stream. Eddy viscosity model is adopted for the calculation of turbulent flows. Turbulent flows on a rotating blade show similar characters as laminar flows. But cross-flow angle of turbulent flows are reduced in comparison with laminar boundary layers. Effects of rotation make flow structures significantly different from two-dimensional flows. In the range of Reynolds number of model scale propellers, large portion of the blade are still in the transition region from laminar to turbulent flows. Therefore viscous flow pattern might be quite different on the blade of model propeller. The present method of calculation is to be useful for the research of scale effects, cavitation, and roughness effects of propeller blades.