• 한국수자원학회논문집
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• 제54권11호
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• pp.985-998
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• 2021

일반적으로 상류의 댐은 하류 유황을 자연 상태에서 발전방류 조건으로 심각하게 변화시킨다. 본 연구에서는 물리서식처모의를 통하여 국내 조절하천에서 자연유황 패턴이 하류의 어류 서식처에 미치는 영향을 조사하였다. 연구 대상하도는 금강의 용담댐 하류 13.4 km 구간으로 설정하였다. 현장조사 결과, 대상하도에서 피라미, 쉬리, 그리고 끄리가 우점하고 있는 것으로 나타났으며, 이들이 전체의 70%를 차지하고 있는 것으로 파악되었다. 이중 끄리는 금강에 서식하는 토착어종이다. 이들 3종을 물리서식처모의를 위한 대상어종으로 선정하였다. 수리해석과 서식처모의를 위하여 2차원 천수방정식에 기반한 Nays2D 모형과 HIS 모형을 각각 사용하였다. 자연 유황에 따른 영향을 검토하기 위하여, 본 연구에서는 댐 유입 유량과 발전유량을 이용하였다. 물리서식처모의 결과, 자연유황 조건에서 대상하도의 복합서식처지수가 크게 증가하는 것으로 나타났다. 그리고 BBA 방법을 이용하여 대상하도에 자연유황에 대한 댐 운영 시나리오를 제시하였다. 시나리오 1을 위하여 유입유량의 양과 지속기간을 고려하는 수문학적 방법을 이용하였고, 시나리오 2는 유입유량을 월별로 평균하여 구축하였다. 시나리오 1과 시나리오 2를 통해서 구현된 자연유황 조건이 발전방류에 비해 가중가용면적을 크게 증가시키는 것으로 나타났다. 결과적으로 댐 운영을 자연유황 조건으로 변환시켜 방류하였을 때 하류의 어류 서식처를 개선하는데 도움이 되는 것으로 확인되었다.

• 한국수자원학회논문집
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• 제44권1호
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• pp.9-22
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• 2011

본 연구에서는 에너지 방정식에 기초하여 정수 식생이 존재하는 자연하도에 적용 가능한 1차원 수치모형을 제시하였다. 수위계산을 위한 마찰경사는 Darcy-Weisbach의 마찰식에 의해 계산되었다. 각 단면의 전체 Darcy-Weisbach 마찰계수는 하상조도높이, 식생, 식생구역과 비식생구역 사이의 전단저항, 그리고 홍수터와 주수로의 경계면 전단저항을 고려하여 산정하였다. 경계면 마찰계수는 Mertens방법과 Nuding방법에 의해 계산되었다. 제시된 모형을 가상하도에 적용하고 HEC-RAS모형 모의결과와 비교, 검증하였고, 식생밀도 등에 대하여 마찰계수의 민감도 분석을 실시하였다. 모형의 적용성검토를 위하여 독일 Enz강 일부구간을 대상으로 수치모의를 실시하고 실측수위와 비교하였다. 식생이 존재하는 Enz강의 실측수위와 계산수위를 비교한 결과 식생의 영향을 거의 받지 않고 주수로에 흐름이 형성되는 저유량의 경우와 식생의 영향을 지배적으로 받는 고유량 흐름 모두에서 합리적인 수위를 예측하여 제시된 모형의 적용 가능성을 확인하였다.

• 대한토목학회논문집
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• 제30권6B호
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• pp.607-615
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• 2010

개수로에 식재된 식생은 항력을 유발하여 유수의 평균유속을 감소시키고 수위를 상승시키는 역할을 한다. 기존 식생수로에 관한 연구는 주로 수직 난류모형에 의한 수직 흐름특성 변화나 1차원 모형에 의한 종방향 흐름특성 변화에 초점을 맞추고 있다. 그러나, 이러한 수치모형을 실제 자연하천에 적용하기란 쉽지 않고, 실무적인 측면에서도 비실용적이다. 따라서, 본 연구에서는 실무적으로 적용성 및 활용도가 높은, 식생항력 개념을 적용시킨, 수심 평균된 2차원 수치모형을 개발하였다. 우선 원주형의 곧은 식생을 가정하여 식생밀도를 정의하고, 식생항력 식을 유도하였으며, 유도된 식생항력 항을 흐름 지배방정식에 추가하여, 식생의 영향을 수치계산에 반영하였다. 개발된 모형의 검증을 위해 단단면 및 복단면 실험수로에서 실측된 수위와 유속 결과를 수치모의 결과와 비교하였으며, 매우 만족스러운 결과를 얻었다. 검증된 모형을 자연하천에 적용하여, 홍수터 식생에 의한 흐름 특성 변화를 모의하여, 식생이 흐름특성에 미치는 영향을 분석하였다.

• Nuclear Engineering and Technology
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• 제56권4호
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• pp.1454-1459
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• 2024

Researchers have applied theoretical and CFD models for years to analyze the fluidelastic instability (FEI) of tube arrays in steam generators and other heat exchangers. The accuracy of each approach has typically been evaluated using the discrepancy between the experimental critical flow velocity and the predicted value. In the best cases, the predicted critical flow velocity was within an order of magnitude comparable to the measured one. This paper revisits the quasi-steady approach for damping controlled FEI in a normal triangular array with a pitch ratio of P/d = 1.375. The method addresses the fluidelastic frequency at the stability threshold as an input parameter for the approach. The excellent agreement between the estimated stability thresholds and the equivalent experimental results suggests that the fluidelastic frequency must be included in the quasi-steady analysis, which requires minimal computing time and experimental data. In addition, the model allows a simple time delay analysis regarding flow convective and viscous effects.

• 한국전산유체공학회지
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• 제15권2호
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• pp.7-13
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• 2010

Flight vehicles such as wheel wells and bomb bays have many cavities. The flow around a cavity is characterized as an unsteady flow because of the formation and dissipation of vortices brought by the interaction between the free stream shear layer and the internal flow of the cavity. The resonance phenomena can damage the structures around the cavity and negatively affect the aerodynamic performance and stability of the vehicle. In this study, a numerical analysis was performed for the cavity flows using the unsteady compressible three-dimensional Reynolds-Averaged Navier-Stokes (RANS) equation with Wilcox's turbulence model. The Message Passing Interface (MPI) parallelized code was used for the calculations by PC-cluster. The cavity has aspect ratios (L/D) of 5.5 ~ 7.5 with width ratios (W/D) of 2 ~ 4. The Mach and Reynolds numbers are 0.4 ~ 0.6 and $1.6{\times}10^6$, respectively. The occurrence of oscillation is observed in the "shear layer and transient mode" with a feedback mechanism. Based on the Sound Pressure Level (SPL) analysis of the pressure variation at the cavity trailing edge, the dominant frequencies are analyzed and compared with the results of Rossiter's formula. The dominant frequencies are very similar to the result of Rossiter's formula and other experimental datum in the low aspect ratio cavity (L/D = ~4.5). In the high aspect ratio cavity, however, there are other low dominant frequencies of the leading edge shear layer with the dominant frequencies of the feedback mechanism.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2009년 추계학술대회논문집
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• pp.13-18
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• 2009

Flight vehicles such as wheel wells and bomb bays have many cavities. The flow around a cavity is characterized as an unsteady flow because of the formation and dissipation of vortices brought about by the interaction between the free stream shear layer and the internal flow of the cavity. The resonance phenomena can damage the structures around the cavity and negatively affect the aerodynamic performance and stability of the vehicle. In this study, a numerical analysis was performed for the cavity flows using the unsteady compressible three-dimensional Reynolds-Averaged Navier-Stokes (RANS) equation with Wilcox's turbulence model. The Message Passing Interface (MPI) parallelized code was used for the calculations by PC-cluster. The cavity has aspect ratios (L/D) of 2.5 ~ 7.5 with width ratios (W/D) of 2 ~ 4. The Mach and Reynolds numbers are 0.4 ~ 0.6 and $1.6{\times}106$, respectively. The occurrence of oscillation is observed in the "shear layer and transient mode" with a feedback mechanism. Based on the Sound Pressure Level (SPL) analysis of the pressure variation at the cavity trailing edge, the dominant frequencies are analyzed and compared with the results of Rossiter's formula. The dominant frequencies are very similar to the result of Rossiter's formula and other experimental data in the low aspect ratio cavity (L/D = ~ 4.5). In the large aspect ratio cavity, however, there are other low dominant frequencies due to the leading edge shear layer with the dominant frequencies of the feedback mechanism. The characteristics of the acoustic wave propagation are analyzed using the Correlation of Pressure Distribution (CPD).

• Nuclear Engineering and Technology
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• 제56권1호
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• pp.233-240
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• 2024

The wall friction correlations of oscillatory natural circulation loops are highly loop-specific, making it difficult to perform 1-D system simulations before obtaining specific experimental data. To better predict the friction characteristics, the nonlinear dynamics of a toroidal single-phase natural circulation loop were numerically investigated, and the transition effect was considered. The k-k_L-ω transitional turbulence and k-ω SST turbulence models were used to compute the flow characteristics of the loop under different heating powers varying from 0.48 to 1.0 W/cm², and the results of both models were compared with previous experiments. The mass flow rates and friction factors predicted by the k-k_L-ω model showed a better agreement with the experimental data than the results of the k-ω SST model. The oscillation frequencies calculated using both models agreed well with the experimental data. The k-k_L-ω transitional turbulence model provided better friction-factor predictions in oscillatory natural circulation loops because it can reproduce the temporal and spatial variation of the wall shear stress more accurately by capturing the movement of laminar, transition turbulent zones inside unstable natural circulation loops. This study shows that transition effects are a possible explanation for the highly loop-specific friction correlations observed in various oscillatory natural circulation loops.

• 한국물환경학회지
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• 제26권5호
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• pp.781-788
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• 2010

A pilot study was performed to examine the feasibility of multiple stage of constructed wetland (CW) for nutrient removal. The system is composed of six wetland cells connected with water-ways. The hydraulic of wetland cells is designed as free water surface flow. The treatment capacity was $25m^3d^{-1}$ at HRT of about one day for each cell. The magnitude of nutrient removal was related with the length of wetlands and plant density. Total N and P removal rates were 1353 and $246mg\;m^{-2}d^{-1}$ respectively. The pilot-scale reactor was model as continuous flow system containing contribution of CSTR and PFR typed-reactors. The $k-C^*$ model equation was applied to predict N and P reduction. The result indicated the equation was well guided to estimate reduction of $NO_3-N$ and $PO_4-P$.

• Journal of Mechanical Science and Technology
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• 제17권1호
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• pp.129-138
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• 2003

A 1 : 20 laboratory scale test rig of a 200 MW tangentially fired boiler is built up with completely simulated structures such as platen heaters and burners. Iso-thermal turbulent flow in the boiler is mapped by 3-D PDA (Particle Dynamic Analyzer). The 3-D numerical models for the same case are proposed based on the solution of к-$\varepsilon$ model closed RANS (Reynolds time-Averaged Navier-Stokes) equations, which are written in the framework of general coordinates and discretized in the corresponding body-fitted meshes. Not only are the grid lines arranged to fit the inner/outer boundaries. but also to align with the streamlines to the best possibility in order to reduce the NDE (numerical diffusion errors). Extensive comparisons of profiles of mean velocities are carried out between experiment and calculation. Predicted velocities in burner region were quantitatively similar with measured ones, while those in other area have same tendency with experimental counterpart.

• 한국수소및신에너지학회논문집
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• 제31권3호
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• pp.314-321
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• 2020

In this work, a preliminary design of an inlet guide vane and runner for developing a 2.5 kW hydraulic turbine was conducted by using computational fluid dynamic analysis. Three-dimensional Reynolds-averaged Navier-Stokes equations with shear stress transport turbulence model were used to analyze the fluid flow in the hydraulic turbine. The hexahedral grid system was used to construct computational domain, and the grid dependency test was performed to obtain the optimal grid system. Velocity triangle diagram considering the flow angles of the inlet guide vane and runner was analyzed to obtain a basic geometry of the inlet guide vane and runner. Through modification of the preliminary design, the hydraulic performances of the turbine have improved under overall drop conditions. Especially, the efficiency and power of the turbine increased by 0.95% and 1.45%, respectively, compared to those of the reference model.