• Proceedings of the Korea Water Resources Association Conference
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• 2016.05a
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• pp.445-445
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• 2016

급변하는 개수로 흐름에서 발생하는 바닥전단응력의 분포는 하천구조물 설계에 있어 매우 중요한 요소이다. 하천 구조물 중 호안에 대한 하천설계기준 '설계편 제 24장 호안'에는 호안 설계에 대한 일반적인 사항이 제시 되어 있으나, 구체적인 소류력 또는 유속에 대한 기준, 각 호안공법들의 안정성을 평가하기 위한 시험법 등에 대한 구체적인 기준이 부족한 상황이다. 소류력 측정방법에는 간접측정법과 직접측정법이 있다. 간접측정법에는 Reach-Average공식, Reynolds Stress, TKE공식 (Turbulent Kinetic Energy)이 있고 직접측정법에는 Shear Meter, Preston Tube 등이 있다. 본 연구에서는 바닥전단응력을 직접 측정할 수 있는 1차원 소류력 측정장치를 개발하고, 최대유속 5m/s 가변형 고속수로 실험을 통하여 Reach-Average 공식, Reynolds Stress, TKE 공식으로 산정한 바닥전단응력 값과 1차원 소류력 측정장치 값을 비교 분석하였다. 실험케이스는 총 3개로, 22.42???, 30.00???, 41.00??? 유량을 사류이면서 난류인 상태로 실험을 수행하였다. 분석 결과, 본 연구에서 개발한 1차원 소류력 측정장치의 측정값은 TKE공식과 약 2.3% 차이가 났으며, Reach-Average공식과 약 8.1%, Reynolds Stress는 약 22.1% 차이가 났다. 즉, 본 연구에서 개발한 1차원 소류력 측정장치는 유속 범위(1m/s ~1.6m/s )에서 TKE공식을 이용한 바닥전단 응력과 가장 근사하게 나타나는 것으로 분석되었다.

• Proceedings of the Korea Water Resources Association Conference
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• 2017.05a
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• pp.384-384
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• 2017

In this study, the numerical investigation of nonlinear flow in a porous medium was carried out. The applied numerical model is ANSYS CFX which is a three-dimensional fluid dynamic model, and the verification of this model was carried out by using the experimental data obtained from Mayer et al works(2011). The experimental and numerical results of velocity and Reynolds number-friction coefficient relationship show relatively a good agreement. Based on the experimental results, we analysed numerically the velocity and Reynolds number-friction coefficient relationship with the variation of permeability, dynamic viscosity and porosity and quantitatively the variation by applying the best curve fitting for each case.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.5 no.1
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• pp.65-74
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• 1985

This study is an experimental analysis for local scour of the riverbed at pier. The basic equation with dimensionless elements(Pier Reynolds Number, Dimensionless Turbulence Intensity) is derived through dimensional analysis. After testing the goodness of fit of data, the coefficients are determined by multiple regression analysis. In the region where the value of the attack angle is near 20 degrees, there exists a transition region where the slope of equation with Pier Reynolds Number changes from positive to negative and that of equation with Dimensionless Turbulence Intensity changes from negative to positive adversely. As a result of testing the equation suggested on this study by using the data of the Institute of National Construction, it is found that the scour depth and width at pier can be predicted approximately.

• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.20 no.2
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• pp.137-142
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• 1984

An experimental study has been performed on the heat transfer characteristics of condensation by the injecting steam flow in the tube. The comparison between results of experimental data and available data concerning equivalent Reynolds number has studied. As the result, the followings were obtained. 1. The shear stress of the radial direction in the tube when the injecting steam flow was condensed can be written as root($\tau$sub(0)/$\tau$sub(0v))=1+1.46X sub(tt) super(0.20). 2. The effect of the heat transfer in the injecting steam flow was less than the value of equivalent Reynolds number. The reason are the nonuniform fluid film of the axial and radial direction in the tube. 3. The value of N sub(u) by the heat transfer of condensation can be written as N sub(u)=1.08$\times$[{$\rho$ sub(l) d/$\mu$ sub(l)}/{$\delta$+(2.5/P sub(rl)) ln(y sub(i)/$\delta$)}]$\times${$\tau$ sub(0)/ $\rho$ sub(l)} super(1/2).

• Proceeding of EDISON Challenge
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• 2015.03a
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• pp.636-641
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• 2015

초소형 비행체는 길이 150mm, 무게 100g 이하의 비행체이다. 초소형 비행체는 그 특성상 저 레이놀즈수에서 비행하며 저 레이놀즈수에서의 공기역학적 특성은 고 레이놀즈수에서의 공기역학적 특성과 큰 차이가 있다. 이는 초소형 비행체 개발 위해 저 레이놀즈수에서의 공력특성 연구가 필요함을 의미한다. 이에 따라 본 연구에서 NACA 4digit Airfoil의 캠버크기와 캠버위치의 변화에 따른 공기역학적 특성의 변화를 확인하였다. 캠버의 위치가 앞전 또는 뒷전으로 이동함에 따라 양력계수가 상승하는 것을 확인하였으며 캠버가 뒷전으로 이동함에 따라 실속이 지연되는 것을 확인하였다. 약 4도 이하의 받음각에서 익형의 아랫변에 발생하는 박리는 고 레이놀즈수에서의 실험에서 확인되어지는 공력특성과 큰 차이를 발생시켰다. 양항비 특성이 가장 우수한 익형은 NACA5808 인 것으로 확인되었다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.21 no.7
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• pp.911-918
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• 1997

The turbulent viscous wake flows behind a single airfoil, two-dimensional stationary blade row and three-dimensional rotating blade row were calculated, and the numerical results were compared with experimental ones. The numerical technique was based on the SIMPLE algorithm using three turbulent closure models, standard k-.epsilon. model(WFM), low Reynolds number k-.epsilon. model(LRN) and Reynolds stress model (RSM). In the case of a single airfoil, WFM, LRN and RSM presented fairly good velocity distributions in the wake compared with experimental data. In the case of the stationary blade row, LRN and RSM presented better results than WFM for wake velocity distribution, and especially LRN showed best results among these three turbulent models. In the case of the rotating blade row, WFM and LRN showed fairly good agreement with experimental data of the three-dimensional velocity component distributions in the range from hub to mid span region. LRN was also superior to WFM in accuracy of prediction for the wake velocity distribution as same with the cases of a airfoil and the stationary blade row.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.22 no.5
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• pp.685-697
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• 1998

Series of recent k-.epsilon. model modification have been carried out with the aid of DNS data to include the effect of near wall. Though these methods opened new way of turbulence modelings, newly developed turbulence models of its kind had yet shortcomings in prediction for the turbulent flows with various Reynolds numbers and various geometric conditions. As a remedy for these shortcomings, a new k-.epsilon. model proposed here by improving the dissipation rate equation and the damping function for eddy viscosity model. The new dissipation rate equation was modeled based on the energy spectrum and magnitude analysis. The damping function for eddy viscosity was also formulated on the ground of distribution of dissipation rate length scales near a wall and the DNS data. The new k-.epsilon. model was applied to the fully developed turbulent flows in a channel and a pipe with a wide range of Reynolds numbers. Prediction results showed that the present model represents properly the turbulence properties in all turbulent regions over a wide range of Reynolds numbers.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.38 no.7
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• pp.557-570
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• 2014

The heat transfer, pressure loss, and thermal performance in a cooling channel were evaluated for various new fan-shaped pin-fin geometries using three-dimensional Reynolds-averaged Navier-Stokes equations. The turbulence was modeled using the low-Reynolds-number SST turbulence model in the Reynolds number range of 5,000-100,000. The numerical results for the area-averaged Nusselt numbers were validated by comparing them with the experimental data under the same conditions. A parametric study for three types of fan-shaped pin-fin geometries was performed with two parameters, namely, the leading and trailing reduction angles.

• 한국가시화정보학회:학술대회논문집
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• 2005.12a
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• pp.54-57
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• 2005

Flow characteristics of hull wake behind a container ship model were investigated experimentally with varying loading condition and Reynolds number. Large-scale bilge vortices of nearly the same strength are formed in the near-wake region. They are symmetric and counter-rotating with respect to the wake centerline for all loading conditions tested. With going downstream for both design and ballast loading conditions, the strength of the bilge vortices decreases and the wake region expands due to diffusion and viscous dissipation. Under the design loading condition, the bilge vortices start to appear at St=0.363 transverse plane above the propeller-boss. For the ballast loading condition, however, the bilge vortices start to appear at St=0.591 below the propeller-boss. They move upward as the hull wake goes downstream and Reynolds number increases. These wake characteristics, under the ballast loading condition, may weaken the propulsion and cavitation performances of the propeller, which are usually optimized for the design loading condition.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.24 no.3
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• pp.382-389
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• 2000

The instantaneous and ensemble averaged flow characteristics of a round jet issuing normally into a crossflow was studied using a flow visualization technique and Particle Image Velocimetry measurements. Experiments were performed at a jet-to-crossflow velocity ratio, 3.3, and two Reynolds numbers, 1050 and 2100, based on crossflow velocity and jet diameter. Instantaneous laser tomographic images of the vertical center plane of the crossflow jet showed that there exist very different natures in the flow structures of the near field jet even though the velocity ratio is the same. It was found that the shear layer becomes much thicker when the Reynolds number is 2100 due to the strong entrainment of the inviscid fluid by turbulent interaction between the jet and crossflow. The mean and second order statistics were calculated by ensemble averaging over 1000 realizations of instantaneous velocity fields. The detail characteristics of mean flow field, stream wise and vertical r.m.s. velocity fluctuations, and Reynolds shear stress distributions were presented. The new PlV results were compared with those from previous experimental and LES studies.