• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2004년도 추계 학술대회논문집
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• pp.111-114
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• 2004

CFD code that simulates stator-rotor interactions is developed applying parallel computing method. Modified Multi-Block Grid System which enhances perpendicularity in grid and is appropriate in parallel processing is introduced and Patched Algorithm is applied in sliding interface which is caused by movement of rotor. The experimental model in the turbo-machine is composed of 11 stators and 14 rotors. Analyses on two test cases which are one stator - one rotor model and three stators - four rotors model are performed. The results of the two cases have been compared with the experimental test data.

• 한국전산구조공학회논문집
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• 제20권3호
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• pp.365-370
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• 2007

공학 및 과학문제 해석을 위해 적용되는 전산 시뮬레이션은 다양한 변수 혹은 데이터의 변화를 통해 다수의 작업을 생성하고 계산함과 동시에, 생성된 결과를 비교 분석하기 위한 필수적인 기법이다. 본 연구에서는 그리드 컴퓨팅을 활용하여 웹상에서 대용량의 전산 시뮬레이션이 가능한 시스템을 개발하고, 이를 이용한 2가지 실제 응용사례를 제시한다. 첫 번째 응용사례는 e-AIRS(Aerospace Integrated Research Environment)라 명명된 연구포탈이다 e-AIRS는 수치해석 연구자가 대규모의 전산 해석을 실시하고, 실험 연구자가 원격지에서 실험을 요청하고 그 결과를 모니터링 할 수 있는 e-Science 연구환경을 제공한다. 두 번째 응용사례는 대규모 계산환경을 이용한 단백질 구조설계를 제시한다. 제안된 계산환경을 이용하여 생성된 단백질 전산 예측구조와 자연상태 구조를 비교하고, 제안된 계산환경의 유용성을 검토한다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2011년도 춘계학술대회 논문집
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• pp.657-662
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• 2011

In this study, aeroelastic performance analyses have been conducted for a 10MW class wind turbine blade model Advanced computational analysis system based on computational fluid dynamics (CFD) and computational structural dynamics (CSD) has been developed in order to investigate detailed dynamic responsed of wind turbine blade Reynolds-averaged Navier-Stokes (RANS) equations with k-${\omega}$ SST turbulence model are solved for unsteady flow problems of the rotating turbine blade model. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3D turbine blade for fluid-structure interaction (FSI) problems.

• 한국정보통신학회논문지
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• 제17권5호
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• pp.1160-1167
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• 2013

네트워크 및 컴퓨팅 기술의 발달로 실생활에서 일어나는 다양한 현상을 수치적으로 계산하고 분석할 수 있는 웹 시뮬레이션 서비스가 활발히 사용되고 있다. 이 논문에서는 웹 기반 열유체 시뮬레이션을 제공하는 e-AIRS(e-Science Aerospace Integrated Research System) 서비스의 개선 및 활용에 대해 기술한다. 2008년부터 서비스된 e-AIRS는 안정성에 일부 문제가 있어 사용자가 종종 원활한 시뮬레이션을 수행하기 어려움이 있었다. 이 문제를 해결하기 위하여 화면 갱신 방법 개선, 서비스 분산처리, 개인별 시뮬레이션 작업량 할당, 데이터 로딩 시간 감소, 등의 개선 작업을 수행하였다. 개선 후 사용자가 110명에서 606명으로 증가했음에도 안정성에 대한 요구사항은 감소하여 효과적으로 개선이 이루어졌음을 알 수 있다. 매 학기마다 분석되는 시뮬레이션 서비스 활용 내역 및 사용자 요구사항은 보다 나은 서비스를 제공하기 위해 사용될 것이다.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.33-36
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• 2006

As the computing environment is rapidly improved, the interests of CFD are gradually focused on large-scale computation over complex geometry. Keeping pace with the trend, essential computational tools to obtain solutions of complex aerospace flow analysis and design problems are examined. An accurate and efficient flow analysis and design codes for large-scale aerospace problem are presented in this work. With regard to original numerical schemes for flow analysis, high-fidelity flux schemes such as RoeM, AUSMPW+ and higher order interpolation schemes such as MLP (Multi-dimensional Limiting Process) are presented. Concerning the grid representation method, a general-purpose basis code which can handle multi-block system and overset grid system simultaneously is constructed. In respect to design optimization, the importance of turbulent sensitivity is investigated. And design tools to predict highly turbulent flows and its sensitivity accurately by fully differentiating turbulent transport equations are presented. Especially, a new sensitivity analysis treatment and geometric representation method to resolve the basic flow characteristics are presented. Exploiting these tools, the capability of the proposed approach to handle complex aerospace simulation and design problems is tested by computing several flow analysis and design problems.

• 한국소음진동공학회논문집
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• 제19권8호
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• pp.764-772
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• 2009

In this study, fluid/structure coupled analyses have been conducted for 3-D stator and rotor configuration. Advanced computational analysis system based on computational fluid dynamics(CFD) and computational structural dynamics(CSD) has been developed in order to investigate fluid/structure responses of general stator-rotor configurations. To solve the fluid/structure coupled problems, fluid domains are modeled using the structural grid system with dynamic moving and local deforming techniques. Reynolds-averaged Navier-Stokes equations with Spalart-Allmaras(S-A) and SST ${\kappa}-{\omega}$ turbulence models are solved for unsteady flow problems. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3-D turbine blades for fluid-structure interaction(FSI) problems. Detailed fluid/structure analysis responses for stator-rotor interaction flow conditions are presented to show the physical performance and flow characteristics.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2008년도 추계학술대회논문집
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• pp.563-569
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• 2008

In this study, fluid/structure coupled analyses have been conducted f3r 3-D stator and rotor configuration. Advanced computational analysis system based on computational fluid dynamics (CFD) and computational structural dynamics (CSD) has been developed in order to investigate fluid/structure responses of general stator-rotor configurations. To solve the fluid/structure coupled problems, fluid domains are modeled using the structural grid system with dynamic moving and local deforming techniques. Reynolds-averaged Navier-Stokes equations with Spalart-Allmaras (S-A) and SST ${\kappa}-{\omega}$ turbulence models are solved for unsteady flow problems. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3-D turbine blades for fluid-structure interaction (FSI) problems. Detailed fluid/structure analysis responses for stator-rotor interaction flow conditions are presented to show the physical performance and flow characteristics.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2009년도 춘계학술대회 논문집
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• pp.652-653
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• 2009

In this study, flow-induced vibration (FIV) analyses have been conducted for a 3D compressor blade model. Advanced computational analysis system based on computational fluid dynamics (CFD) and computational structural dynamics (CSD) has been developed in order to investigate detailed dynamic responses of designed compressor blades. Fluid domains are modeled using the computational grid system with local grid deforming and remeshing techniques. Reynolds-averaged Navier-Stokes equations with $\kappa-\varepsilon$ turbulence model are solved for unsteady flow problems of the rotating compressor model. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3D compressor blade for fluid-structure interaction (FSI) problems. Detailed dynamic responses and instantaneous pressure contours on the blade surfaces considering flow-separation effects are presented to show the multi-physical phenomenon of the rotating compressor blade.

• 한국소음진동공학회논문집
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• 제19권6호
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• pp.551-559
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• 2009

In this study, flow-induced vibration(FIV) analyses have been conducted for a 3D compressor blade model. Advanced computational analysis system based on computational fluid dynamics(CFD) and computational structural dynamics(CSD) has been developed in order to investigate detailed dynamic responses of designed compressor blades. Fluid domains are modeled using the computational grid system with local grid deforming and remeshing techniques. Reynolds-averaged Navier-Stokes equations with $\kappa-\epsilon$ turbulence model are solved for unsteady flow problems of the rotating compressor model. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3D compressor blade for fluid-structure interaction(FSI) problems. Detailed dynamic responses and instantaneous pressure contours on the blade surfaces considering flow-separation effects are presented to show the multi-physical phenomenon of the rotating compressor blade.

• 대한환경공학회지
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• 제29권1호
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• pp.47-53
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• 2007

본 연구의 목적은 대형 석탄 화력 발전소에 DSI(Dry Sorbent Injection)공법 적용 가능성에 대한 연구로서 전산유체역학(CFD; Computational Fluid Dynamics) 기법을 이용하여 N화력 S화력발전 본부에서 운용중인 500MW급 유연탄 발전시설의 보일러 후단에서 전기 집진기 전단까지 덕트 내의 배기가스에 대한 삼차원 유동장에 대한 전산 해석을 수행하였다. CFD상용코드를 이용하여 DSI공법적용 전 기술적 방향을 제시하였는데 덕트의 형상, 탈황제 분사 위치, 분사 속도에 따른 탈황제의 관내 분산 특성에 대한 연구를 중점으로 하였다. 그 결과 DSI공법 적용에 관한 최적의 조건을 확립하였고 그 중 탈황제의 분산에 가장 큰 영향을 미치는 인자는 덕트형상임을 확인하였으며 이에 Lobed-plate라는 탈황제 분산판을 적용한 결과 덕트 내 탈황제의 고른 분산을 유도할 수 있었다.