Full Annulus Simulations of a Transonic Axial Compressor Stage with Distorted Inflow at Transonic and Subsonic Blade Tip Speed

datacite.relatedItem.firstPage7
datacite.relatedItem.issue1
datacite.relatedItem.relatedIdentifierTypeISSN
datacite.relatedItem.relatedItemIdentifier2504-186X
datacite.relatedItem.relationTypeIsPublishedIn
datacite.relatedItem.titleIJTPP
datacite.relatedItem.volume3
dc.contributor.authorJakob Haug
dc.contributor.authorReinhard Niehuis
dc.date.accessioned2024-08-26T12:15:18Z
dc.date.available2024-08-26T12:15:18Z
dc.date.issued2018
dc.identifier.doihttps://doi.org/10.3390/ijtpp3010007
dc.identifier.otherjz000093-0005
dc.identifier.urihttps://tustorage.ulb.tu-darmstadt.de/handle/tustorage/9944
dc.publisherMDPI AG
dc.rights.urihttps://creativecommons.org/licenses/by-nc-nd/4.0/
dc.subject.ddc620
dc.titleFull Annulus Simulations of a Transonic Axial Compressor Stage with Distorted Inflow at Transonic and Subsonic Blade Tip Speed
dc.typeArticle
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