• 신재생에너지
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• 제17권3호
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• pp.1-7
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• 2021

The Korean government announced various energy policies, such as the to reduce 37% of the business-as-usual (BAU) greenhouse gas emissions by 2030. The policies aim to increase the renewable electricity generation ratio to 20% by 2030. PVT is a hybrid technology, which combines photovoltaic (PV) and solar collectors. It is capable of generating electricity and thermal energy simultaneously. It has a great potential to be used as a renewable and clean solar energy. However, there exists a shortage of space for the installation of PVT systems in Korea. To overcome this, in this paper proposes four types of soundproof wall PVT air channels, which were designed and optimized, based on the CFD (Computation Fluid Dynamic) analysis results. The thermal energy generation for multiple PVT units connected in series and pressure drop sensitivity were analyzed, depending on inlet velocity.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.1
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• pp.321-325
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• 2006

Because strong wind is one of the few forces that, although considered in container crane design, still cause significant damage, a container crane was tested to investigate wind load characteristic in uniform flows. So, this study measured an external point pressure at the each members of a container crane according to a wind direction and a shape of members in a wind-tunnel test. The result of this test was compared to those of computation fluid dynamics using a CFX 10. The scale of a container crane model for wind tunnel test applied similarity scales to consider the size of the wind tunnel test section and the boundary condition for CFD is like wind tunnel test.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2011년 춘계학술대회논문집
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• pp.453-457
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• 2011

In this study, transonic aeroelastic response analyses haw been conducted for the business jet aircraft configuration considering shockwave and flow separation effects. The developed fluid-structure coupled analysis system is applied for aeroelastic computations combining computational structural dynamics(CSD), finite element method(FEM) and computational fluid dynamics(CFD) in the time domain. It can give very accurate and useful engineering data on the structural dynamic design of advanced flight vehicles. For the nonlinear unsteady aerodynamics in high transonic flow region, Navier-Stokes equations using the structured grid system have been applied to wing-body configurations. In transonic flight region, the characteristics of static and dynamic aeroelastic responses have been investigated for a typical wing-body configuration model. Also, it is typically shown that the current computation approach can yield realistic and practical results for aircraft design and test engineers.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 춘계학술대회논문집
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• pp.212-215
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• 2008

e-AIRS, an abbreviation of 'e-Science Aerospace Integrated Research System,' is a virtual organization supporting CFD(computational fluid dynamics) simulations, remote experimental service, and collaborative and integrative study between computation and experiment. e-AIRS works on the e-Science environment and research process is accomplished through the web portal. By the system development since 2005, a stable education system with the full support on fluid dynamics is successfully established and utilized to various fluid dynamic lectures in universities. By using e-AIRS system during a lecture, students can conduct the full CFD simulation process on the web and inspect the wind tunnel experiment via Access Grid. This kind of interactive lecture makes students to have a deeper understanding on the physics of fluid, as well as the characteristics of numerical techniques. The current paper will describe system components of e-AIRS and its utilization on education.

• 한국항해항만학회지
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• 제32권1호
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• pp.23-27
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• 2008

컨테이너 크레인의 설계 시 적용되는 하중 조건 중에서 풍하중이 가장 중요하게 고려되어지는바, 본 연구는 75m/s의 풍하중이 컨테이너 크레인에 작용 할 때 컨테이너 크레인의 구조적 안정성에 미치는 영향을 보다 정확하게 예측하기 위하여 유동-구조 연성해석을 실시하였다. 컨테이너 크레인에 작용하는 실제 유동현상을 고려하기 위하여 먼저 전산유동해석을 실시하였으며, 이를 통해서 얻어진 풍하중을 구조해석의 하중조건으로 적용하는 유동-구조 연성해석을 통하여 컨테이너 크레인 각 지지점에서의 반력을 도출하고 그 결과를 분석하였다. 사용된 모델은 주변 환경으로 인하여 컨테이너 크레인의 최대 고도가 제한 될 경우 사용되는 관절형 컨테이너 크레인이며 전산유동해석 및 유동-구조 연성해석 프로그램으로는 ANSYS ICEM CFD 10.0과 ANSYS CFX 10.0을 사용하였다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2011년도 춘계학술대회 논문집
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• pp.299-299
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• 2011

In this study, transonic aeroelastic response analyses have been conducted for the business jet aircraft configuration considering shockwave and flow separation effects. The developed fluid-structure coupled analysis system is applied for aeroelastic computations combining computational structural dynamics(CSD), finite element method(FEM) and computational fluid dynamics(CFD) in the time domain. It can give very accurate and useful engineering data on the structural dynamic design of advanced flight vehicles. For the nonlinear unsteady aerodynamics in high transonic flow region, Navier-Stokes equations using the structured grid system have been applied to wing-body configurations. In transonic flight region, the characteristics of static and dynamic aeroelastic responses have been investigated for a typical wing-body configuration model. Also, it is typically shown that the current computation approach can yield realistic and practical results for aircraft design and test engineers.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2002년도 춘계학술대회논문집
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• pp.89-94
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• 2002

A commercial CFD code is used to calculate the 3-D viscous flow field within the centrifugal pump impeller. Design conditions are changed by impeller inlet(9.3mm, 12.2mm) and outlet breadth(6.65mm, 6.85mm). Numerical calculation was performed by changing flow rate from 8 to 26m$^{3}$/hr. Computation results shows that total head is increased at the larger inlet and outlet breadth than the others. And when the flow rate is increasing, the total head was decreased. The maximum efficiency of pump is shown at the design flow rate(16m$^{3}$/hr). In this study shows that the calculated results are good agreements with analysis results of design condition.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2011년도 추계학술대회 논문집
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• pp.64-71
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• 2011

In this study, steady and unsteady aerodynamic analyses of a huge rocket configuration have been conducted in a transonic flow region. The launch vehicle structural response are coupled with the transonic flow state transitions at the nose of the payload fairing. The developed fluid-structure coupled analysis system is applied for aeroelastic computations combining computational structural dynamics(CSD), finite element method(FEM) and computational fluid dynamics(CFD) in the time domain. It can give very accurate and useful engineering data on the structural dynamic design of advanced flight vehicles. For the nonlinear unsteady aerodynamics in high transonic flow region, Navier-Stokes equations using the structured grid system have been applied to the rocket configurations. Also, it is typically shown that the current computation approach can yield realistic and practical results for rocket design and test engineers.

• 유기물자원화
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• 제19권1호
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• pp.93-101
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• 2011

본 연구는 소각 시스템에 적용되는 반건식 반응기의 모델링 연구를 수행 하였다. 전산유체역학(CFD)을 이용하여 반건식 반응기에서 속도분포 온도분포를 조사하여 반응기의 최적 운전 조건을 조사하였다. 본 모델에 사용된 반응기의 직경은 3 m 이며 높이는 9 m 이다. 반응기로 유입되는 연소가스의 양은 $6,125Nm^3/hr$ 이며 반응기 유입 가스의 온도는 493K 이다. 반응기에 유입되는 소석회 양은 151 kg/hr 이다. 반응기의 입구 형상이 변하면 반응기 내의 온도가 변하며 반응기 내의 가스속도는 0.48 m/sec 에서 1.17m/sec 였으며, 반응기 출구의 가스속도는 6.9에서 7.42m/sec 였다. 모델링 결과에 의하면 반응기 내의 평균 가스 속도와 출구에서의 평균가스 속도는 각각 0.489 m/sec와 7.424 m/sec 였으며, 반응기 출구 온도는 448 K 였다.

• EDISON SW 활용 경진대회 논문집
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• 제3회(2014년)
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• pp.631-636
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• 2014

본 연구는 전산 유체 해석 프로그램인 EDISON_CFD 해석 결과 산출 된 정적공기력계수(양력계수, 항력계수)를 이용하여 교량 단면의 갤로핑(Galloping)에 대한 안정성 평가를 실시하는데 그 목적이 있다. 특히 해상 교량은 장대 교량인데다 높은 풍속까지 견뎌 내야 하므로 내풍 안정성 검토의 중요성이 부각되고 있다. 전산 해석에 사용된 교량은 이순신 대교와 거가 대교의 표준 단면을 사용하였으며, 받음각과 풍속의 변화를 주어 높은 레이놀즈수 영역에서 공기력계수의 변화에 대해 검토하였다.