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    Aerodynamic-Rotordynamic Interaction in Axial Compression Systems—Part I: Modeling and Analysis of Fluid-Induced Forces

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 003::page 405
    Author:
    Ammar A. Al-Nahwi
    ,
    James D. Paduano
    ,
    Samir A. Nayfeh
    DOI: 10.1115/1.1576430
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a first principles-based model of the fluid-induced forces acting on the rotor of an axial compressor. These forces are primarily associated with the presence of a nonuniform flow field around the rotor, such as that produced by a rotor tip clearance asymmetry. Simple, analytical expressions for the forces as functions of basic flow field quantities are obtained. These expressions allow an intuitive understanding of the nature of the forces and—when combined with a rudimentary model of an axial compressor flow field (the Moore-Greitzer model)—enable computation of the forces as a function of compressor geometry, torque and pressure-rise characteristics, and operating point. The forces predicted by the model are also compared to recently published measurements and more complex analytical models, and are found to be in reasonable agreement. The model elucidates that the fluid-induced forces comprise three main contributions: fluid turning in the rotor blades, pressure distribution around the rotor, and unsteady momentum storage within the rotor. The model also confirms recent efforts in that the orientation of fluid-induced forces is locked to the flow nonuniformity, not to tip clearance asymmetry as is traditionally assumed. The turning and pressure force contributions are shown to be of comparable magnitudes—and therefore of equal importance—for operating points between the design point and the peak of the compressor characteristic. Within this operating range, both “forward” and “backward” rotor whirl tendencies are shown to be possible. This work extends recent efforts by developing a more complete, yet compact, description of fluid-induced forces in that it accounts for all relevant force contributions, both tangential and radial, that may influence the dynamics of the rotor. Hence it constitutes an essential element of a consistent treatment of rotordynamic stability under the action of fluid-induced forces, which is the subject of Part II of this paper.
    keyword(s): Force , Pressure , Flow (Dynamics) , Fluids , Compressors , Clearances (Engineering) , Rotors , Blades , Compression AND Aerodynamics ,
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      Aerodynamic-Rotordynamic Interaction in Axial Compression Systems—Part I: Modeling and Analysis of Fluid-Induced Forces

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    http://yetl.yabesh.ir/yetl1/handle/yetl/129233
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    • Journal of Turbomachinery

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    contributor authorAmmar A. Al-Nahwi
    contributor authorJames D. Paduano
    contributor authorSamir A. Nayfeh
    date accessioned2017-05-09T00:11:38Z
    date available2017-05-09T00:11:38Z
    date copyrightJuly, 2003
    date issued2003
    identifier issn0889-504X
    identifier otherJOTUEI-28704#405_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129233
    description abstractThis paper presents a first principles-based model of the fluid-induced forces acting on the rotor of an axial compressor. These forces are primarily associated with the presence of a nonuniform flow field around the rotor, such as that produced by a rotor tip clearance asymmetry. Simple, analytical expressions for the forces as functions of basic flow field quantities are obtained. These expressions allow an intuitive understanding of the nature of the forces and—when combined with a rudimentary model of an axial compressor flow field (the Moore-Greitzer model)—enable computation of the forces as a function of compressor geometry, torque and pressure-rise characteristics, and operating point. The forces predicted by the model are also compared to recently published measurements and more complex analytical models, and are found to be in reasonable agreement. The model elucidates that the fluid-induced forces comprise three main contributions: fluid turning in the rotor blades, pressure distribution around the rotor, and unsteady momentum storage within the rotor. The model also confirms recent efforts in that the orientation of fluid-induced forces is locked to the flow nonuniformity, not to tip clearance asymmetry as is traditionally assumed. The turning and pressure force contributions are shown to be of comparable magnitudes—and therefore of equal importance—for operating points between the design point and the peak of the compressor characteristic. Within this operating range, both “forward” and “backward” rotor whirl tendencies are shown to be possible. This work extends recent efforts by developing a more complete, yet compact, description of fluid-induced forces in that it accounts for all relevant force contributions, both tangential and radial, that may influence the dynamics of the rotor. Hence it constitutes an essential element of a consistent treatment of rotordynamic stability under the action of fluid-induced forces, which is the subject of Part II of this paper.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAerodynamic-Rotordynamic Interaction in Axial Compression Systems—Part I: Modeling and Analysis of Fluid-Induced Forces
    typeJournal Paper
    journal volume125
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1576430
    journal fristpage405
    journal lastpage415
    identifier eissn1528-8900
    keywordsForce
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsFluids
    keywordsCompressors
    keywordsClearances (Engineering)
    keywordsRotors
    keywordsBlades
    keywordsCompression AND Aerodynamics
    treeJournal of Turbomachinery:;2003:;volume( 125 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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