Synergetic effects of thin plies and aligned carbon nanotube interlaminar reinforcement in composite laminates

Author:

Kalfon-Cohen Estelle,Kopp Reed,Furtado Carolina,Ni Xinchen,Arteiro AlbertinoORCID,Borstnar Gregor,Mavrogordato Mark N.,Sinclair Ian,Spearing S. Mark,Camanho Pedro P.,Wardle Brian L.

Funder

National Funds through FCT – Fundação para Ciência e a Tecnologia

U.S. Office of Naval Research

Airbus

Embraer

Lockheed Martin

Saab AB

Hexcel

Saertex

Toho Tenax

ANSYS

MIT's Nano-Engineered Composite aerospace STructures (NECST) Consortium

National Science Foundation

National Science Foundation Graduate Research Fellowship Program

Fundação para a Ciência e a Tecnologia

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference44 articles.

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2. The influence of stacking sequence on laminate strength;Pagano;J. Compos. Mater.,1971

3. Influence of layer thickness on the strength of angle-ply laminates;Herakovich;J. Compos. Mater.,1982

4. K. Kawabe, S. Tomoda, Multi-filament split-yarn sheet and method and device for the manufacture thereof. Patent no. 6032342, USA, 2000.

5. K. Kawabe, S. Tomoda, Method of producing a spread multi-filament bundle and an apparatus used in the same. Patent no. 7832068, USA, 2010.

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