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    Experimental Considerations for Determining the Damping Coefficients of Hard Coatings

    Source: Journal of Aerospace Engineering:;2005:;Volume ( 018 ):;issue: 001
    Author:
    Frank Ivancic
    ,
    Anthony Palazotto
    DOI: 10.1061/(ASCE)0893-1321(2005)18:1(8)
    Publisher: American Society of Civil Engineers
    Abstract: This paper attempts to characterize the various methods that may be used in defining the vibration features of a plate dimensionally proportioned to represent a turbine compressor blade. The comparison is specifically devoted towards certain damping properties of a titanium plate coated with magnesium aluminate spinel (mag spinel). Two different coating thicknesses were tested:
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      Experimental Considerations for Determining the Damping Coefficients of Hard Coatings

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    http://yetl.yabesh.ir/yetl1/handle/yetl/45022
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    contributor authorFrank Ivancic
    contributor authorAnthony Palazotto
    date accessioned2017-05-08T21:16:12Z
    date available2017-05-08T21:16:12Z
    date copyrightJanuary 2005
    date issued2005
    identifier other%28asce%290893-1321%282005%2918%3A1%288%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45022
    description abstractThis paper attempts to characterize the various methods that may be used in defining the vibration features of a plate dimensionally proportioned to represent a turbine compressor blade. The comparison is specifically devoted towards certain damping properties of a titanium plate coated with magnesium aluminate spinel (mag spinel). Two different coating thicknesses were tested:
    publisherAmerican Society of Civil Engineers
    titleExperimental Considerations for Determining the Damping Coefficients of Hard Coatings
    typeJournal Paper
    journal volume18
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2005)18:1(8)
    treeJournal of Aerospace Engineering:;2005:;Volume ( 018 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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