Demonstration of a Crack arresting Concept in Composite Bonded Joints: Testing and Simulation of Carbon Z-Pin Reinforcement Applied to Post-Cured Carbon/Epoxy Laminates-Reference-Cited by-同舟云学术

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Demonstration of a Crack arresting Concept in Composite Bonded Joints: Testing and Simulation of Carbon Z-Pin Reinforcement Applied to Post-Cured Carbon/Epoxy Laminates

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
language:
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Author:

Shor Ofir¹,Grimberg Meirav¹,Simon Ido¹,Poleg Yotam¹,Rev Tamas²,Rittel Daniel²,Shemesh Noam³,Knoth Philip⁴,Clay Stephen B.⁴,Ault Wesley⁵

Affiliation:

1. Rafael Advanced Defense Systems Ltd

2. Technion Israel Institute of Technology

3. IAF Aeronautical Engineering Branch

4. Air Force Research Laboratory

5. Booz Allen Hamilton Inc

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0106

Reference19 articles.

1. Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures

2. Introduction to Aerospace Materials

3. Crack stopping in composite adhesively bonded joints through corrugation

4. Concurrent use of Z-pins for crack arrest and structural health monitoring in adhesive-bonded composite lap joints

5. J. J. Mazza and K. M. Storage, "Bonded Repair in the United States Air Force and Work to Expand Future Capability," pp.1-22.

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