• The Journal of Engineering Geology
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• v.6 no.1
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• pp.1-13
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• 1996

The fracture transmissivity($T_f$) is the most important parameter of fracture in assessing groundwater flow in fractured rock masses by using the DFN(Discrete Fracture Network) modeling. $T_f$, the most sensitive parameter m DFN modeling, is dependent upon aperture, size and filling characteristics of each fracture set. In the field test, the accuracy of $T_f$ can be increased with Borehole Acoustic Scanning (Televiewer) and Fixed Interval Length(FIL) test in constant head. $T_f$ values measured from FIL test was modified and estimated by each fracture set on the basis of the Cubic Law and the information of aperture and filling characteristics obtained from Televiewer. The modified $T_f$ results in the increase of confidence and reliability of modeling results including the amount of tunnel inflow.And, this approach would reduce the uncertaintity of the assessment for groundwater flow in fractured rock masses using the DFN modeling.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.4
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• pp.1-11
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• 2004

Numerical analyses on the aerodynamic characteristics of a counter rotating axial flow fan were conducted for the development of an axial type in-line duct fan. The counter rotating fan has a front rotor and a rear rotor which are counter rotating each other. Blade design of the counter rotating fan was done by extension of design method for axial flow fan which consists of rotor and stator blades. Through flow analysis was performed using matrix method which is applied for flow fields prediction of compressors or turbines. Aerodynamic characteristics and characteristic curves of the counter rotating fan were analyzed by expansion of the frequency domain panel method with duct modeling. Pressure losses were higher at leading edge and hub region of rotor blades. Characteristic curve of the counter rotating fan was overpredicted without consideration of viscous effect.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.5
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• pp.413-422
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• 2012

The ducted fan for a small UAV propulsion can reconnoiter and observe in a town and a small area, it has better thrust efficiency and a long endurance than propeller. Thrust characteristics of hover and for ward flight condition for the ducted fan UAV is important issue to improve a endurance. The unsteady 3-dimensional flow fields of the ducted fan UAV is essential to stable flight. In this paper, to verify the design results of the ducted fan and to investigate a stable aeronautical characteristic, the thrust performance and the unsteady 3-dimensional flow fields are measured. Thrust characteristics for the hovering and the forward flight conditions are measured by the 6-components balance system in the subsonic wind tunnel. The unsteady 3-dimensional flow fields are analyzed by using a stationary $45^{\circ}$ slanted hot-wire technique. The swirl velocity is almost removed behind the stator blades. Therefore, the thrust performance of the ducted fan is improved and the flight stability is maintained.

• Journal of Advanced Marine Engineering and Technology
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• v.34 no.8
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• pp.1094-1099
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• 2010

Three dimensional laminar flows are numerically simulated around the submerged spheres. The finite volume based Navier-Stokes equations with unstructured grids are solved to make clear the hydrodynamic phenomena near and far away from the body. Reviews are made on with the vorticity, velocity, dynamic pressure, residuals, drags, etc. The Reynolds numbers under consideration are 425, 300, 250 and 100. In case of small spacing between spheres, the flow is more stable than that past a single sphere. According to the analysis, the flow past two spheres is found to be unstable as the spacing becomes larger. The rear sphere shows the deduction of stagnation pressure, which results in the decrease of the resistance. The predicted drag coefficients verify that the present numerical calculation is reasonable.

• Proceedings of the Korea Water Resources Association Conference
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• 2021.06a
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• pp.210-210
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• 2021

Delft Dashboard는 유동모델을 위한 오픈소스 프로그램으로 로컬 및 글로벌 데이터 세트를 사용하여 다수의 입력 매개변수를 신속하게 생성, 편집하고 모델 내 입력을 시각화하도록 설계된 그래픽 사용자 인터페이스(GUI) 이다. 특히 Delft Dashboard에 제공하는 개방경계조건을 이용하면 격자영역을 인식하여 개방경계를 자동으로 분배 및 지정하고, 각 개방경계 위치에서 분조별 조석조화상수 값도 산출되므로 유동 모델의 편의성을 증대시킬 수 있지만 상황에 따라 적합하게 경계를 분배하여 개방경계로 지정하는 것이 중요하다. 본 연구에서는 Delft Dashboard에서 제공하는 개방경계조건 중 TPXO 8.0을 이용한 Delft-3D 해수유동 수치모의를 수행하여 개방경계조건이 결과에 미치는 영향을 분석하였다. TPXO 8.0의 경우 격자영역에서 개방경계조건을 설정할 때 사용자가 경계조건에 포함될 격자 수를 지정하면 전체 격자경계에서 격자 수에 해당하는 만큼 경계를 나누어 개방경계를 지정하고 각 개방경계 위치에서의 분조별 조석조화상수값을 산출한다. 특히 격자 수에 따라 개방경계로 지정되는 정도에 따른 영향을 분석하기 위하여 인위적으로 경계를 다양하게 분배하여 개방경계를 지정한 후 수치모의에 적용하였다. 수치모의는 동해안 고리원전 인근을 대상으로 격자 생성 후 Delft Dashboard TPXO 8.0을 이용하여 전술된대로 다양한 개방경계조건을 생성하였고 이를 Delft-3D내 적용하여 해수유동 모의를 수행하였다. 각 개방경계 조건별 초기 수면 변위 분석 및 인근 조위관측소의 관측값의 비교를 통해 개방경계조건이 모의결과에 미치는 영향을 분석하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.1
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• pp.17-25
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• 2019

An intake of Aircraft becomes S-shaped geometry due to spatial limitation or procuring survivability. But curvature of the S-shaped geometry makes secondary flow or flow separation which is the cause of non-uniform pressure distribution. In this study, boundary layer suction is applied to RAE M 2129 S-Duct by attaching sub duct. Design variable is suction location and angle. A mass flow rate drawn out by suction at the sub duct outlet is constant over every model. A grid dependency test was conducted to verify validity of computation. The comparison among the CFD (Computation Fluid Dynamics), ARA experimental result, and ARA computation result of non-dimensional pressure distribution on the Port side and Starboard Side confirmed the validity of CFD. In this study, Distortion Coefficient was used for evaluating aerodynamic performance of S-Duct. The analysis, which was about flow separation, vortex, mass flow rate distribution, and pressure distribution were also investigated. Maximum 26.14% reduction in Distortion Coefficient was verified.

• Journal of the Korean Society of Marine Environment & Safety
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• v.17 no.2
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• pp.167-172
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• 2011

In physical engineering, the turbulent flow on the surface roughness is very important. With the welding, design and paint, the hull surface roughness at each stage in the various aspects are important factors to be considered. In this study, the hull surface roughness geometry that was generalized to the PIV was applied to the tank test. The roughness of the surface changed the distance of the interval. Experimental velocity is Re = $1.1{\times}10^4$, Re = $2.0{\times}10^4$ and Re = $2.9{\times}10^4$. The turbulent intensity at the time-average were examined The roughness coefficient occurred with increasing turbulence intensities was stronger. The turbulence intensity away from the roughness in the shape was zero. The variation of turbulence intensity at the experimental flow conditions change was not affected.

• Water for future
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• v.29 no.3
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• pp.163-176
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• 1996

When a pipe is deployed on a sloping bed, pumping power required for a discharge can be estimated immediately without any iteration process with an explicit form of a friction factor equation. Pumping power being given, however, traditional method requires an iteration process for the solution of discharge and pipe diameter even for the uniformly-rough pipe. You (1955b) has suggested explicit equations for the estimation of discharge and pipe diameter particularly for the cases of pipe on a slopintg bed without pumping and pipe on a horizontal bed with a pumping power. Based on his approach and previous results, the present researchers have developed explicit equations of discharge and pipe diameter for the general case of pipe on a sloping bed with a pumping power. The equations of boundary criteria are also presented in explicit way which render proper choice of various equations suitable for the flow condition between five characteristics. Verification studies are also carried out by applying the explicit equations to a practical example.

• 한국전산유체공학회:학술대회논문집
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• 1998.11a
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• pp.42-47
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• 1998

The pressure-based methods are very popular in CFD because it requires less computer core memory compared to other coupled or density-based solvers. Currently structured-mesh methodology based on pressure-based algorithm is quite mature to apply to the practical problems. The unstructured mesh method needs much more computer memory than the structured-mesh method. However the pressure-based method utilizing the sequential approach does not require very large memory used for unstructured-mesh density-based solvers. The present study has developed the unstructured grid pressure-based method. Cell-centered finite volume method was selected due to robustness for imposing various boundary conditions and easy implementation of higher-order upwind scheme. The predictive capability of present method has validated against several benchmark problems.

• The Korean Journal of Rheology
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• v.10 no.3
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• pp.160-164
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• 1998

본 연구에서 Doi-Edwards 점탄성 조성방정식의 Hadamard 안정성 분석을 행하였 다. Hadamard 안정성은 방정식의 탄성 성질과 연관되는 특성으로 파장이 짧고 진동수가 큰 파동에 의한 외란 하에서 식의 안정성을 의미한다. 먼저 안정성을 위한 일반 3차원 조건을 수립하고 단순한 1차원과 2차원 외란하에서 필요조건을 구하였다. Doi-Edwards 이론을 따 르는 물질의 단순전단유동을 고려함에 의하여 순간 전단변형률이 1.8786을 넘어설 때 파장 이 짧고 진동수가 큰 외란에 의하여 불안정성이 나타남이 증명되었다. 이 안정성의 임계치 는 실제 고분자공정 뿐 아니라 실험실에서도 쉽게 도달할수 있는 값으로 이와 같은 불안정 유동은 mi-crophase separation과 같은 물리적 현상과는 관련이 있다는 증거가 없으므로 조 성방정식 자체가 지니는 수학적 모순점에 기인한 것이라 할수 있다.