Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method

datacite.relatedItem.firstPage441
datacite.relatedItem.issue12
datacite.relatedItem.relatedIdentifierTypeISSN
datacite.relatedItem.relatedItemIdentifier2311-5521
datacite.relatedItem.relationTypeIsPublishedIn
datacite.relatedItem.titleFluids
datacite.relatedItem.volume6
dc.contributor.authorEmanuele Resta
dc.contributor.authorRoberto Marsilio
dc.contributor.authorMichele Ferlauto
dc.date.accessioned2025-04-16T11:32:37Z
dc.date.available2025-04-16T11:32:37Z
dc.date.issued2021
dc.identifier.doihttps://doi.org/10.3390/fluids6120441
dc.identifier.otherjz000105-0271
dc.identifier.urihttps://tustorage.ulb.tu-darmstadt.de/handle/tustorage/14846
dc.publisherMDPI AG
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.subject.ddc530
dc.titleThrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method
dc.typeArticle
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