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

The principal objective of the work is to compare among carbon-glass filament wound epoxy matrix hybrid composites with a different fiber ratio made by robotized winding processes and optimize the geometry suitable for the Rocket Propelled Grenade Launcher. ANSYS based finite element analysis was us...

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Detalles Bibliográficos
Autores principales: Mishra, Rajesh, Behera, Bijoy Kumar, Mukherjee, Sayan, Petru, Michal, Muller, Miroslav
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2021
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7915840/
https://www.ncbi.nlm.nih.gov/pubmed/33572252
http://dx.doi.org/10.3390/polym13040517

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7915840/
https://www.ncbi.nlm.nih.gov/pubmed/33572252
http://dx.doi.org/10.3390/polym13040517

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