Low velocity impact and pseudo-ductile behaviour of carbon/glass/epoxy and carbon/glass/PMMA hybrid composite laminates for aircraft application at service temperature-Reference-Cited by-同舟云学术

Low velocity impact and pseudo-ductile behaviour of carbon/glass/epoxy and carbon/glass/PMMA hybrid composite laminates for aircraft application at service temperature

Published:2020-09 Issue: Volume:89 Page:106711
ISSN:0142-9418
Container-title:Polymer Testing
language:en
Short-container-title:Polymer Testing

Author:

Subadra Sharath P.,Griskevicius Paulius,Yousef Samy

Funder

Kaunas University of Technology

Publisher

Elsevier BV

Subject

Polymers and Plastics,Organic Chemistry

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4. Experimental investigation of woven E-glass epoxy composite laminates subjected to low-velocity impact at different energy levels;Mathivanan;J. Miner. Mater. Char. Eng.,2010

5. Mechanical and low-velocity impact properties of epoxy-composite beams reinforced by MWCNTs;Ranjbar;J. Compos. Mater.,2019

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