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

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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Bibliographic Details
Main Authors: Rajesh Mishra, Bijoy Kumar Behera, Sayan Mukherjee, Michal Petru, Miroslav Muller
Format: Article
Language:English
Published: MDPI AG 2021-02-01
Series:Polymers
Subjects:
carbon fibers
glass fibers
mechanical properties
finite element analysis (FEA)
filament winding
Online Access:https://www.mdpi.com/2073-4360/13/4/517

Internet

https://www.mdpi.com/2073-4360/13/4/517

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