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dc.contributor.authorKushwaha, Abhishek
dc.contributor.authorKasthuri, Praveen
dc.contributor.authorPawar, Samadhan A.
dc.contributor.authorSujith, R. I.
dc.contributor.authorChterev, Ianko
dc.contributor.authorBoxx, Isaac
dc.date.accessioned2023-11-29T18:43:24Z
dc.date.available2023-11-29T18:43:24Z
dc.date.copyright8/1/2023 12:00:00 AM
dc.date.issued8/1/2023 12:00:00 AM
dc.date.issued2023-08-01
dc.identifier.issn0742-4795
dc.identifier.othergtp_145_10_107001.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4294342
dc.description.abstractThe following are the changes made to the original paper:1. Section 2 (Experimental setup) Last paragraph third sentence -For each combination of thermal load and equivalence ratio, the fraction of hydrogen in the fuel was varied in increments of 10%, until flashback occurred or the thermoacoustic pulsations were strong enough to damage the combustor windows. In total, 48 flame conditions were successfully measured.2. Section 2 (Experimental Setup) Table 1 column 3 -
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleErratum: “Dynamical Characterization of Thermoacoustic Oscillations in a Hydrogen-Enriched Partially Premixed Swirl-Stabilized Methane/Air Combustor” [ASME J. Eng. Gas Turbines Power, 143(12), p. 121022; DOI: 10.1115/1.4052091]
dc.typeJournal Paper
dc.journal.volume145
dc.journal.issue10
dc.journal.titleJournal of Engineering for Gas Turbines and Power
dc.identifier.doi10.1115/1.4062841
dc.journal.fristpage107001-1
dc.journal.lastpage107001-3
dc.page3
dc.treeJournal of Engineering for Gas Turbines and Power:;2023:;volume( 145 ):;issue: 010
dc.contenttypeFulltext


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