• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2004년도 추계 학술대회논문집
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• pp.101-104
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• 2004

CFD simulation is peformed for 2D and 3D frisbees flying at 10m/s. For convenience of simulation, rotation of 3D model is not considered. CFD results show that pitching moment makes the nose down and holes at the leading and trailing edges improve the lift characteristics of the frisbee.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2006년도 PARALLEL CFD 2006
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• pp.121-125
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• 2006

CFD has been used in aircraft development and broaden its influence in various fields of industries. This paper briefly introduces the historical trends of computing system, the overview of CFD applications in Korean Supersonic Trainer Development Program and the demand for CFD software in industry points of view.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.962-967
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• 2003

CFD data compression method based on supercompact multiwavelets is presented. High data compression can be achieved when taking advantage of the compact nature of multiwavelets. Thresholding technique is also a matter of primary concern in determining pressure ratio. In this paper, we apply thresholding for multiwavelets that considers the coefficient vector as a whole rather than thresholding individual elements. Various thresholding methods are described briefly. CFD data compression suggests that the multivariate thresholding method is suitable for supercompact multiwavelets.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 1999년도 유체기계 연구개발 발표회 논문집
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• pp.147-160
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• 1999

The importance of CFD work in the process of turbomachinery development has been continuously growing. It is therefore necessary to have some bench marks for validation purposes when any CFD codes are to be developed. In the present study, some public information on centrifugal compressor test results is collected to render useful data for the developers.

• Nuclear Engineering and Technology
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• 제42권4호
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• pp.377-381
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• 2010

In 2007 the Nuclear Energy Agency's Committee on the Safety of Nuclear Installations published Best Practice Guidelines for the use of CFD in Nuclear Reactor Safety. This paper provides an overview of the document' contents and highlights a few of its recommendations. The document covers the full extent of a CFD analysis from initial problem definition and selection of an appropriate tool for the analysis, through final documentation of results. It provides advice on selection of appropriate simulation software, mesh construction, and selection of physical models. In addition it contains extensive discussion of the verification and validation process that should accompany any high-quality CFD analysis.

• 대한원격탐사학회지
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• 제36권6_3호
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• pp.1643-1652
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• 2020

본 연구에서는 국지예보시스템(LDAPS)과 전산유체역학(CFD) 모델을 접합하여, 부산 중구 광복동에 소재한 건물 밀집 지역의 상세 흐름을 조사하였다. 도시 지역 기상에 대한 보다 현실적인 수치 모의를 위해 기상청이 현업으로 운용하는 LDAPS 결과로부터 기상 요소(풍향, 풍속, 온위)를 추출하여 CFD 모델의 초기·경계장으로 사용하였다. LDAPS로부터 추출한 기상 요소(U, V)는 공간 선형 보간법을 이용하여 CFD 모델의 수평·연직 격자에 맞게 내삽하였고, 공간 선형 보간법을 이용해 내삽한 온위는 CFD 모델의 각 격자점에서 온도로 변환된다. 본 연구에서는 건물 옥상에서 측정한 3차원 초음파 풍향·풍속계에서 측정한 풍속과 풍향을 이용하여 수치 모의 결과를 검증하였다. 대상 기간(2020년 6월 22일) 동안 측정 지점(PKNU-SONIC)에서는 바람이 약하게 나타났고, 새벽 시간에는 북동풍과 북서풍이 불었으며, 주간에는 주로 남동풍이 불었다. LDAPS-CFD 접합 모델은 측정 풍향과 풍속을 유사하게 수치 모의하였다. 07시에는 동북동쪽에서 유입되는 흐름이 지형과 건물에 의해 변화하였고, PKNU-SONIC 지점에서 수치 모의된 풍향(동남동풍)은 측정 풍향과 유사하다. 19시에는 남동쪽에서 유입되는 흐름이 PKNU-SONIC 지점까지 유입되어 측정 풍향과 유사하게 모의하였다.

• 한국항공우주학회지
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• 제45권1호
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• pp.10-20
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• 2017

본 연구는 기존 Flow Angularity 장착물 분리 풍동시험 기법을 전산유체해석(Computational Fluid Dynamics)에 적용하여 해석 결과로부터 유동각 데이터베이스를 구성하고 6자유도 분리 궤적 해석한 결과를 전산유체해석의 CTS(Captive Trajectory Simulation) 해석 결과와 비교하여 CFD 해석 기법의 적용 가능성을 확인 한 것이다. Flow Angularity 기법의 전산유체해석 결과는 항공기와 외장간의 각 위치들에서 획득된 공력계수 데이터와 비교하여 데이터의 적절성을 확인하였다. 또한 Flow Angularity 기법으로 획득된 전산유체해석 데이터로부터 획득된 6자유도 외장 분리 궤적과 전산유체해석으로 해석한 CTS 외장분리 궤적을 비교하여 해석 기법의 적용 가능성을 확인하였다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2010년 춘계학술대회논문집
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• pp.320-325
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• 2010

A multiphase CFD analysis is performed to investigate the effect of near-wall grid for simulating a subcooled boiling flow in vertical tube. The multiphase flow model used in this CFD analysis is the two-fluid model in which liquid(water) and vapor(steam) are considered as continuous and dispersed fluids, respectively. A wall boiling model is also used to simulate the subcooled boiling heat transfer at the heated wall boundary. The diameter and heated length of tube are 0.0154 m and 2 m, respectively. The system pressure in tube is 4.5 MPa and the inlet subcooling is 60 K. The near-wall grid size in the non-dimensional wall unit ($y_{w}^{+}$) was examined from 64 to 172 at the outlet boundary. The CFD calculations predicted the void distributions as well as the liquid and wall temperatures in tube. The predicted axial variations of the void fraction and the wall temperature are compared with the measured ones. The CFD prediction of the wall temperature is shown to slightly depend on the near-wall grid size but the axial void prediction has somewhat large dependency. The CFD prediction was found to show a better agreement with the measured one for the large near-wall grid, e.g., $y_{w}^{+}$ > 100.

• 항공우주기술
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• 제9권1호
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• pp.35-41
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• 2010

고속으로 비행하는 물체는 공력가열에 의해 온도가 상승한다. KSLV-I 비행 중 공력가열 조건을 예측하는 방법으로 MINIVER를 이용하는 방법과 전산유동해석(CFD)기법을 이용하는 방법이 있다. MINIVER는 경험적 기법을 이용하여 대류열전달계수 및 회복온도를 산출하며, CFD 기법은 실제 유동장을 해석하여 발사체 표면에서의 공력가열조건을 산출한다. 본 연구에서는 CFD 기법을 이용하여 얻은 공력가열조건을 PLF 구조물 외부 표면에 적용하여 PLF 내부 온도장을 해석하고 그 결과를 KSLV-I 1차 비행시험 결과와 비교하였다.

• 국제초고층학회논문집
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• 제8권2호
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• pp.107-116
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• 2019

The use of computational fluid dynamics (CFD) is becoming an increasingly popular means to model wind flows in and around buildings. The first published application of CFD to both indoor and outdoor building airflows was in the 1970's. Since then, CFD usage has expanded to include different aspects of building design. Wind tunnel testing (WTT) on buildings for wind loads goes back as far as 1908. Gustave Eiffel built a pair of wind tunnels in 1908 and 1912. Using these he published wind loads on an aircraft hangar in 1919 as cited in Hoerner (1965 - page 74). The second of these wind tunnels is still in use today for tests including building design ($Damljanovi{\acute{c}}$, 2012). The Empire State Building was tested in 1933 in smooth flow - see Baskaran (1993). The World Trade Center Twin Towers in New York City were wind tunnel tested in the mid-sixties for both wind loads, at Colorado State University (CSU) and the [US] National Physical Laboratory (NPL), as well as pedestrian level winds (PLW) at the University of Western Ontario (UWO) - Baskaran (1993). Since then, the understanding of the planetary boundary layer, recognition of the structures of turbulent wakes, instrumentation, methodologies and analysis have been continuously refined. There is a drive to replace WTT with computational methods, with the rationale that CFD is quicker, less expensive and gives more information and control to the architects. However, there is little information available to building owners and architects on the limitations of CFD for flows around buildings and communities. Hence building owners, developers, engineers and architects are not aware of the risks they incur by using CFD for different studies, traditionally conducted using wind tunnels. This paper will explain what needs to happen for CFD to replace wind tunnels. Ultimately, we anticipate the reader will come to the same conclusion that we have drawn: both WTT and CFD will continue to play important roles in building and infrastructure design. The most pressing challenge for the design and engineering community is to understand the strengths and limitations of each tool so that they can leverage and exploit the benefits that each offers while adhering to our moral and professional obligation to hold paramount the safety, health, and welfare of the public.