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dc.contributor.authorFuqua, Matthew N.
dc.contributor.authorRutledge, James L.
dc.date.accessioned2022-02-06T05:52:01Z
dc.date.available2022-02-06T05:52:01Z
dc.date.copyright6/15/2021 12:00:00 AM
dc.date.issued2021
dc.identifier.issn0889-504X
dc.identifier.otherturbo_143_11_111003.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4278938
dc.description.abstractThe classical method of superposition has been used for several decades to provide an estimate of the adiabatic effectiveness for multiple sets of already well-characterized film cooling hole rows. In this way, design work is aided by classical superposition theory prior to higher fidelity experiments or simulations that would account for fluid dynamic interaction for which superposition cannot account. In the present work, we consider the additive effects of multiple rows of coolant holes, but now also with coolant issuing at different temperatures. There are a number of ways that coolant may issue from different cooling hole rows at different temperatures, one of which is simply the necessarily different internal channels through which the coolant must pass. The film cooling effectiveness is investigated for double rows of cooling holes wherein the two rows have different coolant temperatures. A double row consisting of an upstream slot and a downstream row of 7–7–7 cooling holes were first evaluated with a single coolant temperature to demonstrate that classical superposition theory applies well to the present configuration. Superposition theory is then extended to the context of multiple coolant temperatures and a new nondimensional parameter is identified, which governs cooling performance. The theory is experimentally evaluated by independently varying the coolant temperatures of the two rows. Circumstances are identified in which the second row of cooling holes may be detrimental to cooling performance.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleFilm Cooling Superposition Theory for Multiple Rows of Cooling Holes With Multiple Coolant Temperatures
dc.typeJournal Paper
dc.journal.volume143
dc.journal.issue11
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.4051001
dc.journal.fristpage0111003-1
dc.journal.lastpage0111003-12
dc.page12
dc.treeJournal of Turbomachinery:;2021:;volume( 143 ):;issue: 011
dc.contenttypeFulltext


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