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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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