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

Date
2021-01-01
Authors
Journal Title
Journal ISSN
Volume Title
Publisher
MDPI
Abstract
Description
Subject(s)
carbon fibers, glass fibers, mechanical properties, finite element analysis (FEA), filament winding
Citation
Item identifier
https://dspace.tul.cz/handle/15240/161656
 https://doi.org/10.3390/polym13040517
ISSN
2073-4360
ISBN
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