The Influence of Combustor Swirl on Pressure Losses and the Propagation of Coolant Flows at the Large Scale Turbine Rig (LSTR): Experimental and Numerical Investigation

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datacite.relatedItem.firstPage12
datacite.relatedItem.issue3
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datacite.relatedItem.relatedItemIdentifier2504-186X
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datacite.relatedItem.titleIJTPP
datacite.relatedItem.volume2
dc.contributor.authorHolger Werschnik
dc.contributor.authorMarius Schneider
dc.contributor.authorJanina Herrmann
dc.contributor.authorDimitri Ivanov
dc.contributor.authorHeinz-Peter Schiffer
dc.contributor.authorChristoph Lyko
dc.date.accessioned2024-08-26T12:17:34Z
dc.date.available2024-08-26T12:17:34Z
dc.date.issued2017
dc.identifier.doihttps://doi.org/10.3390/ijtpp2030012
dc.identifier.otherjz000100-0013
dc.identifier.urihttps://tustorage.ulb.tu-darmstadt.de/handle/tustorage/10038
dc.publisherMDPI AG
dc.rights.urihttps://creativecommons.org/licenses/by-nc-nd/4.0/
dc.subject.ddc620
dc.titleThe Influence of Combustor Swirl on Pressure Losses and the Propagation of Coolant Flows at the Large Scale Turbine Rig (LSTR): Experimental and Numerical Investigation
dc.typeArticle
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