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dc.contributor.authorPelz, Peter F.
dc.contributor.authorSaul, Sebastian
dc.contributor.authorBrötz, Johannes
dc.date.accessioned2022-05-08T08:55:44Z
dc.date.available2022-05-08T08:55:44Z
dc.date.copyright1/28/2022 12:00:00 AM
dc.date.issued2022
dc.identifier.issn0889-504X
dc.identifier.otherturbo_144_6_061001.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284520
dc.description.abstractThe efficiency, pressure ratio, and shaft power of a fan depends on type, size, working medium, and operating condition. For acceptance tests, a dissimilarity in Reynolds number, Mach number, relative roughness, and relative blade tip clearance of the scaled model and prototype is unavoidable. Hence, the efficiency differs between model and prototype. This difference is quantified by scaling methods. This article presents a validated and physics based, i.e., reliable scaling method for the efficiency, pressure ratio, and shaft power of axial and centrifugal fans operating at subsonic conditions. The method is validated using test results gained on standardized test rigs for different fan types, sizes, and operating conditions. For all scenarios, the presented scaling method provides a much reduced scaling uncertainty compared to the reference method described in ISO 13348.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleEfficiency Scaling: Influence of Reynolds and Mach Numbers on Fan Performance
dc.typeJournal Paper
dc.journal.volume144
dc.journal.issue6
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.4053172
dc.journal.fristpage61001-1
dc.journal.lastpage61001-12
dc.page12
dc.treeJournal of Turbomachinery:;2022:;volume( 144 ):;issue: 006
dc.contenttypeFulltext


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