Axial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validation

Simple item page
dc.contributor.authorPetrů Michalcs
dc.date.accessioned2022-01-29T18:14:35Z
dc.date.available13-06-2021en
dc.date.available2022-01-29T18:14:35Z
dc.date.issued2021-01-01cs
dc.format.extent18cs
dc.identifier.doi10.3390/polym13040517
dc.identifier.issn2073-4360cs
dc.identifier.urihttps://dspace.tul.cz/handle/15240/161656
dc.language.isoengcs
dc.publisherMDPIcs
dc.publisher.cityBaselcs
dc.relation.ispartofPolymersen
dc.relation.ispartofseries1cs
dc.relation.urihttps://www.mdpi.com/2073-4360/13/4/517/htmcs
dc.subjectcarbon fiberscs
dc.subjectglass fiberscs
dc.subjectmechanical propertiescs
dc.subjectfinite element analysis (FEA)cs
dc.subjectfilament windingcs
dc.titleAxial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validationcs
local.citation.epage1-18cs
local.citation.spage1-18cs
local.identifier.publikace8353
local.relation.issue4cs
Files
Collections