Thermoelastic constants of symmetric laminates with cracks in 90-layer: application of simple models-Reference-Cited by-同舟云学术

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Thermoelastic constants of symmetric laminates with cracks in 90-layer: application of simple models

Published:2013-05 Issue:4 Volume:42 Page:157-166
ISSN:1465-8011
Container-title:Plastics, Rubber and Composites
language:en
Short-container-title:Plastics, Rubber and Composites

Author:

Loukil M S¹,Hussain W¹,Kirti A¹,Pupurs A¹,Varna J¹

Affiliation:

1. Division of Polymer EngineeringLuleå University of Technology, Luleå, Sweden

Publisher

Maney Publishing

Subject

Materials Chemistry,Polymers and Plastics,General Chemical Engineering,Ceramics and Composites

Link

https://www.tandfonline.com/doi/pdf/10.1179/1743289811Y.0000000064

Reference16 articles.

1. Highsmith AL, Reifsnider KL: ‘Damage in composite materials’, ASTM STP 775’; 1982, Philadelphia, PA, ASTM.

2. Ply cracking and property degradations of symmetric balanced laminates under general in-plane loading

3. Poisson's ratio as a damage parameter in the static tensile loading of simple crossply laminates

4. Prediction of Transverse Cracking and Stiffness Reduction in Cross-Ply Laminated Composites

5. Analytical modeling of stiffness reduction in symmetric and balanced laminates due to cracks in 90° layers

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1. Experimental Characterization and Modeling of 3D Printed Continuous Carbon Fibers Composites with Different Fiber Orientation Produced by FFF Process;Polymers;2022-01-21

2. A computational study about the effects of ply cracking and delamination on the stiffness reduction of damaged lamina and laminate;International Journal of Damage Mechanics;2021-08-13

3. Microcracking in thermally cycled and aged Carbon fibre/polyimide laminates;International Journal of Fatigue;2017-01

4. Strategies for stiffness analysis of laminates with microdamage: combining average stress and crack face displacement based methods;ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik;2015-06-29

5. Damage evolution modelling in laminates;Structural Integrity and Durability of Advanced Composites;2015

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