TY - GEN
T1 - Biaxial fatigue damage in quasi isotropic laminates
AU - Skinner, Travis
AU - Datta, Siddhant
AU - Chattopadhyay, Aditi
AU - Hall, Asha
N1 - Funding Information:
Research was sponsored by the Army Research Laboratory and was accomplished under Cooperative Agreement W911NF-17-2-0207. The views and conclusions contained in this document are those of the authors and should not be interpreted as representing the official policies, either expressed or implied, of the Army Research Laboratory or the U.S. Government. The U.S. Government is authorized to reproduce and distribute reprints for Government purposes notwithstanding any copyright notation herein.
Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Copyright:
Copyright 2021 Elsevier B.V., All rights reserved.
PY - 2020
Y1 - 2020
N2 - An investigation into the biaxial fatigue damage mechanisms in quasi isotropic carbon fiber reinforced polymer (CFRP) composite laminates has been conducted. The goal is to capture early stage damage and obtain an improved understanding of the physics of damage and failure under complex multiaxial loading in anisotropic laminates. Specimen geometry is designed using an optimization technique and digital image correlation (DIC) is performed during static biaxial load tests to validate specimen design. To understand the propagation of damage from the micro-to the macroscale, the fractured surfaces are analyzed during various stages of fatigue using scanning electron microscope (SEM) assisted fractography, and a high-resolution camera is used to capture real time macroscale damage. Specimen stiffness degradation is measured and correlated to the micro-and macroscale damage mechanisms and the biaxial fatigue loading parameters. The results provide critical understanding of the initiation and propagation of damage mechanisms in quasi isotropic laminates under biaxial fatigue.
AB - An investigation into the biaxial fatigue damage mechanisms in quasi isotropic carbon fiber reinforced polymer (CFRP) composite laminates has been conducted. The goal is to capture early stage damage and obtain an improved understanding of the physics of damage and failure under complex multiaxial loading in anisotropic laminates. Specimen geometry is designed using an optimization technique and digital image correlation (DIC) is performed during static biaxial load tests to validate specimen design. To understand the propagation of damage from the micro-to the macroscale, the fractured surfaces are analyzed during various stages of fatigue using scanning electron microscope (SEM) assisted fractography, and a high-resolution camera is used to capture real time macroscale damage. Specimen stiffness degradation is measured and correlated to the micro-and macroscale damage mechanisms and the biaxial fatigue loading parameters. The results provide critical understanding of the initiation and propagation of damage mechanisms in quasi isotropic laminates under biaxial fatigue.
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U2 - 10.2514/6.2020-0475
DO - 10.2514/6.2020-0475
M3 - Conference contribution
AN - SCOPUS:85084848137
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -