• 제목/요약/키워드: FSI Method

검색결과 171건 처리시간 0.022초

동심축 이중관 구조에서 유동기인진동 특성 고찰 (Investigation of FIV Characteristics on a Coaxial Double-tube Structure)

  • 송기남;김용완;박상철
    • 대한기계학회논문집A
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    • 제33권10호
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    • pp.1108-1118
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    • 2009
  • A Very High Temperature Gas Cooled Reactor (VHTR) has been selected as a high energy heat source of the order of $950^{\circ}C$ for nuclear hydrogen generation, which can produce hydrogen from water or natural gas. A primary hot gas duct (HGD) as a coaxial double-tube type cross vessel is a key component connecting a reactor pressure vessel and an intermediate heat exchanger in the VHTR. In this study, a structural sizing methodology for the primary HGD of the VHTR is suggested in order to modulate a flow-induced vibration (FIV). And as an example, a structural sizing of the horizontal HGD with a coaxial double-tube structure was carried out using the suggested method. These activities include a decision of the geometric dimensions, a selection of the material, and an evaluation of the strength of the coaxial double-tube type cross vessel components. Also in order to compare the FIV characteristics of the proposed design cases, a fluid-structure interaction (FSI) analysis was carried out using the ADINA code.

조립식 클립형 비닐하우스의 강풍 및 폭설시 구조 안정성 평가 (An Evaluation of the Structural Stability of a Clip Type Prefabricated Greenhouse under Strong Wind and Heavy Snow Conditions)

  • 노경철
    • 한국산학기술학회논문지
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    • 제15권6호
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    • pp.3423-3428
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    • 2014
  • 본 연구는 폭설 및 강풍 시 조립식 비닐하우스의 구조안정성을 해석하였으며, 내재해 규격 중 가장 엄격한 기준인 적설량 40 cm, 풍속 40m/s를 재해 기준으로 고려하여 적설 하중 및 풍 하중이 비닐하우스 구조에 미치는 영향을 분석하였다. 풍 하중의 경우, 공기역학적 특성에 의해 비닐하우스의 형상에 따른 국부적인 압력 분포 특성이 상이하기 때문에 유체-고체연성 해석 기법을 적용하였다. 적설하중 및 풍하중 해석 결과에서 비닐하우스 하단지지 파이프와 지붕서까래 체결 부분 근처에서 가장 큰 응력 및 변형이 발생하며, 적설 하중에 비해 풍 하중 시 구조 안정성이 다소 취약함을 확인하였다. 따라서 본 연구 결과를 기반으로 지지 파이프의 변형을 최소화 하면서 설치 및 유지보수가 용이한 조립식 연결 클립 설계를 위한 기초자료로 활용할 예정이다.

Arbitrary Lagrange-Eulerian 기법을 활용한 액중 방전 성형의 해석적 연구 (Numerical Study of Electrohydraulic Forming Using an Arbitrary Lagrange-Eulerian Method)

  • 우민아;노학곤;송우진;강범수;김정
    • 소성∙가공
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    • 제25권1호
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    • pp.49-55
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    • 2016
  • Electrohydraulic forming (EHF) is a high-speed forming process that uses an electric arc discharge in water. Shock waves resulting from the electric arc discharge are propagated to the blank through water and the blank moves toward the die. Advantages of EHF include improved formability due to the high-speed process and reduction of the bouncing effect. In the current study, a numerical simulation of EHF was developed using LS-DYNA. In the simulation, the model for the electric arc was assumed as an adiabatic gas expansion and an Arbitrary Lagrange-Eulerian (ALE) multi material formulation was used to describe the interaction between the electric arc and the water. In order to model the Fluid-Structure Interaction (FSI), a coupling mechanism was used. The blank of Al 1100-O was simulated using shell elements. The results of the simulation showed that the blank was deformed due to the pressure propagation of water and the bouncing effect did not affect the formability of blank.

회전과 유동박리효과를 고려한 3차원 풍력발전 터빈 블레이드의 공탄성 응답 해석 (Aeroelastic Response Analysis of 3D Wind Turbine Blade Considering Rotating and Flow Separation Effects)

  • 김동현;김요한;김동만;김유성;황미현
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2009년도 춘계학술대회 논문집
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    • pp.68-75
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    • 2009
  • In this study, aeroelastic response analyses have been conducted for a 3D 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. Vibration analyses of rotating wind-turbine blade have been conducted using the general nonlinear finite element program, SAMCEF (Ver.6.3). Reynolds-averaged Navier-Stokes (RANS)equations with spalart-allmaras 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. Detailed dynamic responses and instantaneous Mach contour on the blade surfaces considering flow-separation effects are presented to show the multi-physical phenomenon of the rotating wind-turbine blade model.

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A Numerical Analysis on the Curved Bileaflet Mechanical Heart Valve (MHV): Leaflet Motion and Blood Flow in an Elastic Blood Vessel

  • Bang, Jin-Seok;Choi, Choeng-Ryul;Kim, Chang-Nyung
    • Journal of Mechanical Science and Technology
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    • 제19권9호
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    • pp.1761-1772
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    • 2005
  • In blood flow passing through the mechanical heart valve (MHV) and elastic blood vessel, hemolysis and platelet activation causing thrombus formation can be seen owing to the shear stress in the blood. Also, fracture and deformation of leaflets can be observed depending on the shape and material properties of the leaflets which is opened and closed in a cycle. Hence, comprehensive study is needed on the hemodynamics which is associated with the motion of leaflet and elastic blood vessel in terms of fluid-structure interaction. In this paper, a numerical analysis has been performed for a three-dimensional pulsatile blood flow associated with the elastic blood vessel and curved bileaflet for multiple cycles in light of fluid-structure interaction. From this analysis fluttering phenomenon and rebound of the leaflet have been observed and recirculation and regurgitation have been found in the flow fields of the blood. Also, the pressure distribution and the radial displacement of the elastic blood vessel have been obtained. The motion of the leaflet and flow fields of the blood have shown similar tendency compared with the previous experiments carried out in other studies. The present study can contribute to the design methodology for the curved bileaflet mechanical heart valve. Furthermore, the proposed fluid-structure interaction method will be effectively used in various fields where the interaction between fluid flow and structure are involved.

3차원 축류압축기 블레이드의 유체유발진동 해석 (Flow-Induced Vibration (FIV) Analysis of a 3D Axial Compressor Blade)

  • 김동현;김유성;;정규강;김경희;민대기
    • 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.

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3차원 축류압축기 블레이드의 유체유발진동 해석 (Flow-induced Vibration(FIV) Analysis of a 3D Axial Compressor Blade)

  • 김동현;김유성;;정규강;김경희;민대기
    • 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.

Comparative study on the resistance performance of an icebreaking cargo vessel according to the variation of waterline angles in pack ice conditions

  • Kim, Moon-Chan;Lee, Won-Joon;Shin, Yong-Jin
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제6권4호
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    • pp.876-893
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    • 2014
  • The resistance performance of an icebreaking cargo vessel according to the variation of waterline angles is investigated numerically and experimentally. A recently developed Finite Element (FE) model is used in our analysis. A resistance test with synthetic ice is performed in the towing tank at Pusan National University (PNU) to compare and validate the computed results. We demonstrate good agreement between the experimental and numerical results. Shipice interaction loads are numerically calculated based on the Fluid Structure Interaction (FSI) method in the commercial FE package LS-DYNA. Test results from model testing with synthetic ice at the PNU towing tank are used to compare and validate the numerical simulations. For each waterline angle, numerical and experimental comparisons were made for three concentrations (90%, 80%, and 60%) of pack ice. Ice was modeled as a rigid body, but the ice density was the same as that used in the experiments. A comparative study according to the variation of stem angles is expected to be conducted in the near future.

Influence of Impact from Anti-Aircraft Bullet on Rotorcraft Fuel Tank Assembly

  • Kim, Sung Chan;Kim, Hyun Gi
    • International Journal of Aerospace System Engineering
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    • 제5권1호
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    • pp.1-8
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    • 2018
  • Military rotorcrafts are constantly exposed to risk from bullet impacts because they operate in a battle environment. Because bullet impact damage can be deadly to crews, the fuel tanks of military rotorcraft must be designed taking extreme situations into account. Fuel tank design factors to be considered include the internal fluid pressure, the structural stress on the part impacted, and the kinetic energy of bullet strikes. Verification testing using real objects is the best way to obtain these design data effectively, but this imposes substantial burdens due to the huge cost and necessity for long-term preparation. The use of various numerical simulation tests at an early design stage can reduce the risk of trial-and-error and improve the prediction of performance. The present study was an investigation of the effects of bullet impacts on a fuel tank assembly using numerical simulation based on SPH (smoothed particle hydrodynamics), and conducted using the commercial package, LS-DYNA. The resulting equivalent stress, internal pressure, and kinetic energy of the bullet were examined in detail to evaluate the possible use of this numerical method to obtain configuration design data for the fuel tank assembly.

디퓨저 베인에 의한 공진조건에서의 임펠러 구조 안정성 평가 (Structural Stability Evaluation of Impeller in Resonant condition due to Diffuser vanes)

  • 김용세;공동재;신상준;임강수;박기훈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.877-880
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    • 2017
  • 원심압축기 임펠러의 블레이드는 고속회전과 정상유동 압력에 의한 정적하중이 가해진다. 동시에 임펠러와 디퓨저 베인 간 상호작용에 의해 발생하는 비정상 유동의 공력가진력이 공진조건에서 주기적으로 임펠러를 가진함에 따라 임펠러 블레이드의 고주기피로 파손이 발생할 수 있다. 이에 대한 정밀한 구조응답 예측을 위해 ANSYS를 이용한 비정상 유동 해석과 모드해석을 각기 수행하여 공력가진력과 주요 공진조건을 도출하였다. 이 후 공력-구조를 연계하는 단일방향의 강제진동 해석을 수행하고, 결과들을 토대로 고주기피로에 대한 안전도를 평가하였다.

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