On mode-I and mode-II interlaminar crack migration and R-curves in carbon/epoxy laminates with hybrid toughening via core-shell rubber particles and thermoplastic micro-fibre veils-Reference-Cited by-同舟云学术

On mode-I and mode-II interlaminar crack migration and R-curves in carbon/epoxy laminates with hybrid toughening via core-shell rubber particles and thermoplastic micro-fibre veils

Published:2022-06 Issue: Volume:238 Page:109900
ISSN:1359-8368
Container-title:Composites Part B: Engineering
language:en
Short-container-title:Composites Part B: Engineering

Author:

Akbolat Mehmet Çağatay^ORCID,Katnam Kali Babu,Soutis Constantinos^ORCID,Potluri Prasad,Sprenger Stephan,Taylor James

Funder

Ministerio de Educación de la Nación

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference68 articles.

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4. Impact damage tolerance of thermoset composites reinforced with hybrid commingled yarns;Selver;Compos B Eng,2016

5. Progress in interlaminar toughening of aerospace polymer composites using particles and non-woven veils;İnal;Aeronaut J,2021

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