Numerical Simulation of Folding Tail Aeroelasticity Based on the CFD/CSD Coupling Method

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datacite.relatedItem.firstPage705
datacite.relatedItem.issue3
datacite.relatedItem.relatedIdentifierTypeISSN
datacite.relatedItem.relatedItemIdentifier2571-631X
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datacite.relatedItem.titleVibration
datacite.relatedItem.volume7
dc.contributor.authorDi Zhou
dc.contributor.authorWeitao Lu
dc.contributor.authorJiangpeng Wu
dc.contributor.authorTongqing Guo
dc.contributor.authorBinbin Lv
dc.contributor.authorHongtao Guo
dc.contributor.authorHongya Xia
dc.date.accessioned2025-05-21T17:19:08Z
dc.date.available2025-05-21T17:19:08Z
dc.date.issued2024
dc.identifier.doihttps://doi.org/10.3390/vibration7030037
dc.identifier.otherjz000175-0037
dc.identifier.urihttps://tustorage.ulb.tu-darmstadt.de/handle/tustorage/36130
dc.publisherMDPI AG
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.subject.ddc620
dc.titleNumerical Simulation of Folding Tail Aeroelasticity Based on the CFD/CSD Coupling Method
dc.typeArticle
dcat.distribution.pdfhttps://tustorage.ulb.tu-darmstadt.de/handle/tustorage/36131
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2024