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    Accelerating the Calibration of Multihole Pressure Probes by Applying Advanced Computational Methods

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 003::page 425
    Author:
    Arnoud R. C. Franken
    ,
    Paul C. Ivey
    DOI: 10.1115/1.1791285
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The miniature multihole pneumatic pressure probe is widely regarded as a cost-effective, easy-to-use, and accurate method for performing two- or three-dimensional flow field measurements in turbomachinery. The major downside to the use of these probes is that the influence of fabrication imperfections on probe characteristics necessitates an extensive and highly time-intensive and, therefore, costly calibration of each individual probe. Unless these probes can be fabricated to such standards that make individual probe calibrations superfluous, the only way to significantly reduce the time and costs associated with probe calibration is to shorten the calibration process. The latter is only possible if all essential information can be obtained from less calibration data. This paper describes an approach to the calibration of a series of multihole pressure probes in which advanced computational methods are used to make this possible. By exploiting the key features of a probe’s characteristic this approach requires only a fraction of the size of a conventional calibration database for the accurate modeling of the relationships between port pressures and flow conditions. As a result, calibration time and costs can be reduced without the sacrifice of quality.
    keyword(s): Calibration , Probes , Yaw , Computational methods , Pressure , Flow (Dynamics) AND Mach number ,
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      Accelerating the Calibration of Multihole Pressure Probes by Applying Advanced Computational Methods

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/132778
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    • Journal of Turbomachinery

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    contributor authorArnoud R. C. Franken
    contributor authorPaul C. Ivey
    date accessioned2017-05-09T00:18:06Z
    date available2017-05-09T00:18:06Z
    date copyrightJuly, 2005
    date issued2005
    identifier issn0889-504X
    identifier otherJOTUEI-28721#425_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/132778
    description abstractThe miniature multihole pneumatic pressure probe is widely regarded as a cost-effective, easy-to-use, and accurate method for performing two- or three-dimensional flow field measurements in turbomachinery. The major downside to the use of these probes is that the influence of fabrication imperfections on probe characteristics necessitates an extensive and highly time-intensive and, therefore, costly calibration of each individual probe. Unless these probes can be fabricated to such standards that make individual probe calibrations superfluous, the only way to significantly reduce the time and costs associated with probe calibration is to shorten the calibration process. The latter is only possible if all essential information can be obtained from less calibration data. This paper describes an approach to the calibration of a series of multihole pressure probes in which advanced computational methods are used to make this possible. By exploiting the key features of a probe’s characteristic this approach requires only a fraction of the size of a conventional calibration database for the accurate modeling of the relationships between port pressures and flow conditions. As a result, calibration time and costs can be reduced without the sacrifice of quality.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAccelerating the Calibration of Multihole Pressure Probes by Applying Advanced Computational Methods
    typeJournal Paper
    journal volume127
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1791285
    journal fristpage425
    journal lastpage430
    identifier eissn1528-8900
    keywordsCalibration
    keywordsProbes
    keywordsYaw
    keywordsComputational methods
    keywordsPressure
    keywordsFlow (Dynamics) AND Mach number
    treeJournal of Turbomachinery:;2005:;volume( 127 ):;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
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