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    Humidity Effects on Experimental Compressor Performance—Corrected Conditions for Real Gases

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 003::page 31011
    Author:
    Berdanier, Reid A.
    ,
    Smith, Natalie R.
    ,
    Fabian, John C.
    ,
    Key, Nicole L.
    DOI: 10.1115/1.4028356
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of humid air on the performance of a multistage research compressor and new methods of humidity accounting to ensure appropriate representation of performance parameters are investigated in this paper. Turbomachinery textbooks present methods of correcting speed and mass flow rate using perfect gas assumptions, but these methods can reduce the ability to achieve repeatable compressor performance when using unconditioned air in a climate where absolute humidity may vary. Instead, a new method is introduced, which models humid air as a real gas and circumvents the need for assumptions in the correction process. In the area of compressor research, the ability to measure small changes in performance parameters and ensure repeatable results is essential. Errors of more than 0.5% can result from using perfect gas assumptions to calculate corrected speed, which can lead to misrepresented performance parameters beyond the uncertainty of the measurements. Multiplicative correction factors based on analytical data are also introduced as an alternate method of applying the new realgas method, and these correction factors are compared to those derived by previous authors applying ideal gas methods for humidity accounting. This is the first time in open literature that experimental results for a component of a gas turbine engine are presented comparing a humid air correction method with traditional correction methods.
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      Humidity Effects on Experimental Compressor Performance—Corrected Conditions for Real Gases

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    http://yetl.yabesh.ir/yetl1/handle/yetl/159899
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    contributor authorBerdanier, Reid A.
    contributor authorSmith, Natalie R.
    contributor authorFabian, John C.
    contributor authorKey, Nicole L.
    date accessioned2017-05-09T01:24:27Z
    date available2017-05-09T01:24:27Z
    date issued2015
    identifier issn0889-504X
    identifier otherturbo_137_03_031011.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159899
    description abstractThe effects of humid air on the performance of a multistage research compressor and new methods of humidity accounting to ensure appropriate representation of performance parameters are investigated in this paper. Turbomachinery textbooks present methods of correcting speed and mass flow rate using perfect gas assumptions, but these methods can reduce the ability to achieve repeatable compressor performance when using unconditioned air in a climate where absolute humidity may vary. Instead, a new method is introduced, which models humid air as a real gas and circumvents the need for assumptions in the correction process. In the area of compressor research, the ability to measure small changes in performance parameters and ensure repeatable results is essential. Errors of more than 0.5% can result from using perfect gas assumptions to calculate corrected speed, which can lead to misrepresented performance parameters beyond the uncertainty of the measurements. Multiplicative correction factors based on analytical data are also introduced as an alternate method of applying the new realgas method, and these correction factors are compared to those derived by previous authors applying ideal gas methods for humidity accounting. This is the first time in open literature that experimental results for a component of a gas turbine engine are presented comparing a humid air correction method with traditional correction methods.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHumidity Effects on Experimental Compressor Performance—Corrected Conditions for Real Gases
    typeJournal Paper
    journal volume137
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4028356
    journal fristpage31011
    journal lastpage31011
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 003
    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
    yabeshDSpacePersian