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dc.contributor.authorBanjac, Milan
dc.contributor.authorPetrovic, Milan V.
dc.contributor.authorWiedermann, Alexander
dc.date.accessioned2022-02-06T05:53:06Z
dc.date.available2022-02-06T05:53:06Z
dc.date.copyright5/17/2021 12:00:00 AM
dc.date.issued2021
dc.identifier.issn0889-504X
dc.identifier.otherturbo_143_7_077001.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4278978
dc.description.abstractIn the published paper, the expressions listed under (51) were miswritten. The correct version is (51)–for a rotor:–for a stator:(w2/w1)T<Ctc(WRmin)T/1.3(w2/w1)A<(WRmin)A(w2/w1)H<(WRmin)H/1.3(w2/w1)T<(WRmin)T/1.3(w2/w1)A<(WRmin)A(w2/w1)H<Ctc(WRmin)H/1.3And the following sentence should be: “Hub and tip minimum velocity ratios are divided by a factor of 1.3 due to the ability of the blade row to operate stably in spite of the presence of corner stall.”
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleErratum: “Secondary Flows, Endwall Effects, and Stall Detection in Axial Compressor Design” [ASME J. Turbomach. 2015, 137(5), p. 051004; DOI: 10.1115/1.4028648]
dc.typeJournal Paper
dc.journal.volume143
dc.journal.issue7
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.4049916
dc.journal.fristpage077001-1
dc.journal.lastpage077001-1
dc.page1
dc.treeJournal of Turbomachinery:;2021:;volume( 143 ):;issue: 007
dc.contenttypeFulltext


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