• 항공우주기술
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• 제3권1호
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• pp.35-44
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• 2004

본 연구에서는 액체로켓에 쓰이는 터보펌프 부분흡입현 터빈의 1차원 공력계산 및 구조설계에 대해 고찰하였다. 터빈은 노즐, 로터, 후방유도익등으로 나누어 각각에 대해 공력 특성을 계산식으로부터 유도하였고 CFD 계산을 통해 그 타당성을 입증하였다. 속도삼각형과 같은 1차원 설계 변수들은 평균선 방정식을 이용하여 수행되었고 2-D, 3-D CFD 계산을 통해 보정되었다. 블레이드 익형은 CFD 최적화기법을 통해 결정되었다. 향후, 열응력계산, 구조응력계산을 통한 열적/구조적 거동에 대해 연구가 필요하다.

• Wind and Structures
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• 제9권6호
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• pp.473-492
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• 2006

This paper presents numerical results of pedestrian-level wind environment around the base of a row of tall buildings by CFD. Four configurations of building arrangement are computed including a single square tall building. Computed results of pedestrian-level wind flow patterns and wind speeds are compared to previous wind tunnel measurement data to enable an assessment of CFD predictions. The CFD model uses the finite-volume method with RNG $k-{\varepsilon}$ model for turbulence closure. It is found that the numerical results can reproduce key features of pedestrian-level wind environment such as corner streams around corners of upwind building, sheltered zones behind buildings and channeled high-speed flow through a building gap. However, there are some differences between CFD results and wind tunnel data in the wind speed distribution and locations of highest wind speeds inside the corner streams. In locations of high ground-level wind speeds, CFD values match wind tunnel data within ${\pm}10%$.

• 한국항공우주학회지
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• 제45권3호
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• pp.191-193
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• 2017

EFD-CFD 비교워크샵은 AIAA의 Drag Prediction Workshop과 High Lift Prediction Workshop을 참고하여 국내의 풍동실험과 전산해석기술 수준을 향상시키고 두 분야의 협력을 통해 공기역학의 기술수준을 고양하고자 조직되었다. 국내외에서 수행된 3개의 풍동실험 Case에 대한 전산해석 수행 및 비교분석을 수행하며 2015년부터 비교 워크샵이 개최되고 있다. 향후 국내 연구자들의 참여와 협력을 적극 유도하며 새로운 형상에 대한 실험과 해석 및 분석을 진행하여 국내 공기역학의 기술발전에 기여하고자 한다.

• 한국분무공학회지
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• 제19권3호
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• pp.123-129
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• 2014

A diesel spray overall SMD (Sauter mean diameter) in a spray chamber was simulated with CFD by varying the compression ratio in the spray chamber from 18:1 to 100:1. The gas densities of the spray chambers for the compression ratios of 18:1 and 100:1 were 17.97 and $74.8kg/m^3$, respectively. Standard KIVA-3V code was used for the CFD simulation. Various fuel injection patterns such as single injection, pilot injection and split injection were used for the CFD simulation. Fuel injection pressures for the simulated diesel sprays are 90 and 120 MPa. As the compression ratio increases, the CFD simulated SMD was decreased, which was generally in agreement with previous experimental studies.

• International Journal of Fluid Machinery and Systems
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• 제2권4호
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• pp.400-408
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• 2009

Optimization of seal geometries can reduce significantly the energetic losses in a hydraulic seal [1], especially for high head runner turbine. In the optimization process, a reliable prediction of the losses is needed and CFD is often used. This paper presents numerical experiments to determine an adequate CFD model for straight, labyrinth and stepped hydraulic seals used in Francis runners. The computation is performed with a finite volume commercial CFD code with a RANS low Reynolds turbulence model. As numerical computations in small radial clearances of hydraulic seals are not often encountered in the literature, the numerical results are validated with experimental data on straight seals and labyrinth seals. As the validation is satisfactory enough, geometrical optimization of hydraulic seals using CFD will be studied in future works.

• International Journal of Naval Architecture and Ocean Engineering
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• 제3권1호
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• pp.65-71
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• 2011

Seakeeping analysis has progressed from the linear frequency-domain 2D strip method to the nonlinear timedomain 3D panel method. Nevertheless, the violent free surface flows such as slamming and green water on deck are beyond the scope of traditional panel methods based on potential theory. Recently, Computational Fluid Dynamics (CFD) has become an attractive numerical tool that can effectively deal with the violent free surface flows. ABS, as a classification society, is putting forth a significant amount of effort to implement the CFD technology to the advanced strength assessment of modern commercial ships and high-speed naval craft. The main objective of this study is to validate the CFD technology as a seakeeping tool for ship design considering fully nonlinear three-dimensional slamming and green water on deck. The structural loads on a large container carrier were successfully calculated from the CFD analysis and validated with segmented model test measurements.

• 설비공학논문집
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• 제16권2호
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• pp.111-120
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• 2004

The optimal design method of indoor thermal environment using CFD coupled simulation and genetic algorithms (GA) is developed in this study. CFD could analyze the thermal environment considering the distribution of temperature, velocity, etc. in a room. Therefore, It would be appropriate to use CFD for the optimal design method considering their distribution. In this paper, the optimal design means the most appropriate boundary conditions of the room among the conditions where the design target of indoor therm environment is achieved. Two step optimal indoor thermal environment design method is proposed. It includes the GA for searching the optimal indoor thermal environment design. To examine the performance of this method, the optimal design of hybrid ventilation system, which uses the natural cross ventilation and the radiation-cooling panel is conducted. The optimal design which satisfies the design target (thermal comfort, minimum cooling load, minimum vertical temperature difference) is found using two step optimal design method.

• Nuclear Engineering and Technology
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• 제53권7호
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• pp.2162-2173
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• 2021

In this paper, the coupling of fine-mesh computational fluid dynamics (CFD) thermal-hydraulics (TH) code and neutronics code is achieved using the Ansys Fluent User Defined Function (UDF) for code development, including parallel meshing mapping, data computation, and data transfer. Also, some CFD schemes are designed for mesh mapping and data transfer to guarantee physical conservation in the coupling computation. Because there is no rigorous research that gives robust guidance on the various CFD schemes that must be obtained before the fine-mesh coupling computation, this work presents a quantitative analysis of the CFD meshing and mapping schemes to improve the accuracy of the value and location of key physical prediction. Furthermore, the effect of the sub-pin scale coupling computation is also studied. It is observed that even the pin-resolved coupling computation can also create a large deviation in the maximum value and spatial locations, which also proves the significance of the research on mesh mapping and data transfer for CFD code in a coupling computation.

• International Journal of Naval Architecture and Ocean Engineering
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• 제6권2호
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• pp.269-281
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• 2014

This paper examines the suitability of using the Computational Fluid Dynamics (CFD) tools, ANSYS-CFX, as an initial analysis tool for predicting the drag and propulsion performance (thrust and torque) of a concept underwater vehicle design. In order to select an appropriate thruster that will achieve the required speed of the Underwater Disk Robot (UDR), the ANSYS-CFX tools were used to predict the drag force of the UDR. Vertical Planar Motion Mechanism (VPMM) test simulations (i.e. pure heaving and pure pitching motion) by CFD motion analysis were carried out with the CFD software. The CFD results reveal the distribution of hydrodynamic values (velocity, pressure, etc.) of the UDR for these motion studies. Finally, CFD bollard pull test simulations were performed and compared with the experimental bollard pull test results conducted in a model basin. The experimental results confirm the suitability of using the ANSYS-CFX tools for predicting the behavior of concept vehicles early on in their design process.

• 한국컴퓨터정보학회논문지
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• 제28권1호
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• pp.121-127
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• 2023

본 연구에서는 질소화합물을 최적으로 줄일 수 있는 SCR에서 설계 조건과 CFD 해석 결과를 비교해 검토하고자 한다. 이를 위해 보일러의 쉘과 튜브 영역에 대해 설계 기준을 만족하고 있는지 CFD을 이용하여 해석하고 비교하였다. SCR 시스템에서 해석영역은 쉘 측은 가스·공기 열교환기 입구에서 출구까지이고, 튜브 측은 가스·공기 열교환기의 8개 튜브로 설정하였다. CFD 해석을 통해 SCR 시스템의 1차 촉매 면에서 가스의 속도 분포는 2.7%로 설계되었고, NH3/NOx 몰비 분포는 3.7%로 설계 기준을 만족하였다. 또한, 온도 분포의 균일성을 확인하였고 요구 조건인 260℃ 이상을 만족하였다. 촉매에 유입되는 가스의 각도는 2.9도로 설계 조건을 충족하였고, 그리고 발생하는 압력손실도 설계 요구조건을 만족하였다. 이러한 CFD 해석을 통해 각 영역별로 요구되는 설계조건을 만족하여 설계되어 최적으로 운전되고 있음을 확인하였다.