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    Engine Dynamic Analysis With General Nonlinear Finite-Element Codes, Part 1: Overall Approach and Development of Bearing Damper Element

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003::page 586
    Author:
    M. L. Adams
    ,
    J. Padovan
    ,
    D. G. Fertis
    DOI: 10.1115/1.3227320
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: There is currently a considerable interest and level of activity in developing computational schemes to predict general engine dynamic behavior. The general feeling among researchers working on engine vibration problems is that various modes of operation, such as blade-loss events, require a high level of analysis sophistication to realistically model the engine. Proper account of system nonlinearities (particularly at the bearings, dampers and rubs) appears to be necessary if analytical predictions are to be realistic. The approach described in this paper seeks to make use of already proven general finite-element nonlinear time-transient computer codes which are available on the open market. The work specifically described in this paper covers the first phase of a three-phase NASA-Lewis-sponsored research grant on engine dynamic simulation with available finite element codes. The first phase was concentrated on the development of a bearing-damper element computer software package suitable for “plug-in” to available finite element codes.
    keyword(s): Bearings , Dampers , Dynamic analysis , Finite element analysis , Engines , Simulation , Vibration , Computers , Blades AND Computer software ,
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      Engine Dynamic Analysis With General Nonlinear Finite-Element Codes, Part 1: Overall Approach and Development of Bearing Damper Element

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/95760
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. L. Adams
    contributor authorJ. Padovan
    contributor authorD. G. Fertis
    date accessioned2017-05-08T23:13:11Z
    date available2017-05-08T23:13:11Z
    date copyrightJuly, 1982
    date issued1982
    identifier issn1528-8919
    identifier otherJETPEZ-26776#586_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95760
    description abstractThere is currently a considerable interest and level of activity in developing computational schemes to predict general engine dynamic behavior. The general feeling among researchers working on engine vibration problems is that various modes of operation, such as blade-loss events, require a high level of analysis sophistication to realistically model the engine. Proper account of system nonlinearities (particularly at the bearings, dampers and rubs) appears to be necessary if analytical predictions are to be realistic. The approach described in this paper seeks to make use of already proven general finite-element nonlinear time-transient computer codes which are available on the open market. The work specifically described in this paper covers the first phase of a three-phase NASA-Lewis-sponsored research grant on engine dynamic simulation with available finite element codes. The first phase was concentrated on the development of a bearing-damper element computer software package suitable for “plug-in” to available finite element codes.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEngine Dynamic Analysis With General Nonlinear Finite-Element Codes, Part 1: Overall Approach and Development of Bearing Damper Element
    typeJournal Paper
    journal volume104
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227320
    journal fristpage586
    journal lastpage593
    identifier eissn0742-4795
    keywordsBearings
    keywordsDampers
    keywordsDynamic analysis
    keywordsFinite element analysis
    keywordsEngines
    keywordsSimulation
    keywordsVibration
    keywordsComputers
    keywordsBlades AND Computer software
    treeJournal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003
    contenttypeFulltext
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