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    Analysis of Fluid-Structure Interaction by Means of Dynamic Unstructured Meshes

    Source: Journal of Fluids Engineering:;1998:;volume( 120 ):;issue: 004::page 792
    Author:
    F. J. Blom
    ,
    P. Leyland
    DOI: 10.1115/1.2820740
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a computational analysis on forced vibration and fluid-structure interaction in compressible flow regimes. A so-called staggered approach is pursued where the fluid and structure are integrated in time by distinct solvers. Their interaction is then taken into account by a coupling algorithm. The unsteady fluid motion is simulated by means of an explicit time-accurate solver. For the fluid-structure interaction problems which are considered here the effects due to the viscosity can be neglected. The fluid is hence modeled by the Euler equations for compressible inviscid flow. Unstructured grids are used to discretise the fluid domain. These grids are particularly suited to simulate unsteady flows over complex geometries by their capacity of being dynamically refined and unrefined. Dynamic mesh adaptation is used to enhance the computational precision with minimal CPU and memory constraints. Fluid-structure interaction involves moving boundaries. Therefore the Arbitrary Lagrange Euler method (ALE-method) is adopted to solve the Euler equations on a moving domain. The deformation of the mesh is controlled by means of a spring analogy in conjunction with a boundary correction to circumvent the principle of Saint Venant. To take advantage of the differences between fluid and structure time scales, the fluid calculation is subcycled within the structural time step. Numerical results are presented for large rotation, pitching oscillation and aeroelastic motion of the NACA0012 airfoil. The boundary deformation is validated by comparing the numerical solution for a flat plate under supersonic flow with the analytical solution.
    keyword(s): Fluid structure interaction , Fluids , Motion , Equations , Deformation , Inviscid flow , Airfoils , Oscillations , Rotation , Flat plates , Springs , Supersonic flow , Unsteady flow , Viscosity , Algorithms , Vibration , Accuracy AND Compressible flow ,
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      Analysis of Fluid-Structure Interaction by Means of Dynamic Unstructured Meshes

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    https://yetl.yabesh.ir/yetl1/handle/yetl/120580
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    contributor authorF. J. Blom
    contributor authorP. Leyland
    date accessioned2017-05-08T23:56:53Z
    date available2017-05-08T23:56:53Z
    date copyrightDecember, 1998
    date issued1998
    identifier issn0098-2202
    identifier otherJFEGA4-27134#792_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120580
    description abstractThis paper presents a computational analysis on forced vibration and fluid-structure interaction in compressible flow regimes. A so-called staggered approach is pursued where the fluid and structure are integrated in time by distinct solvers. Their interaction is then taken into account by a coupling algorithm. The unsteady fluid motion is simulated by means of an explicit time-accurate solver. For the fluid-structure interaction problems which are considered here the effects due to the viscosity can be neglected. The fluid is hence modeled by the Euler equations for compressible inviscid flow. Unstructured grids are used to discretise the fluid domain. These grids are particularly suited to simulate unsteady flows over complex geometries by their capacity of being dynamically refined and unrefined. Dynamic mesh adaptation is used to enhance the computational precision with minimal CPU and memory constraints. Fluid-structure interaction involves moving boundaries. Therefore the Arbitrary Lagrange Euler method (ALE-method) is adopted to solve the Euler equations on a moving domain. The deformation of the mesh is controlled by means of a spring analogy in conjunction with a boundary correction to circumvent the principle of Saint Venant. To take advantage of the differences between fluid and structure time scales, the fluid calculation is subcycled within the structural time step. Numerical results are presented for large rotation, pitching oscillation and aeroelastic motion of the NACA0012 airfoil. The boundary deformation is validated by comparing the numerical solution for a flat plate under supersonic flow with the analytical solution.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of Fluid-Structure Interaction by Means of Dynamic Unstructured Meshes
    typeJournal Paper
    journal volume120
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2820740
    journal fristpage792
    journal lastpage798
    identifier eissn1528-901X
    keywordsFluid structure interaction
    keywordsFluids
    keywordsMotion
    keywordsEquations
    keywordsDeformation
    keywordsInviscid flow
    keywordsAirfoils
    keywordsOscillations
    keywordsRotation
    keywordsFlat plates
    keywordsSprings
    keywordsSupersonic flow
    keywordsUnsteady flow
    keywordsViscosity
    keywordsAlgorithms
    keywordsVibration
    keywordsAccuracy AND Compressible flow
    treeJournal of Fluids Engineering:;1998:;volume( 120 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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