Corrigendum to

Overcoming the cohesive zone limit in composites delamination: modeling with slender structural elements and higher-order adaptive integration (International Journal for Numerical Methods in Engineering, (2020), 121, 24, (5511-5545), 10.1002/nme.6497)

Journal Article (2022)
Author(s)

Raffaele Russo (TU Delft - Aerospace Structures & Computational Mechanics)

B. Chen (TU Delft - Aerospace Structures & Computational Mechanics)

Research Group
Aerospace Structures & Computational Mechanics
Copyright
© 2022 R. Russo, B. Y. Chen
DOI related publication
https://doi.org/10.1002/nme.6938
More Info
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Publication Year
2022
Language
English
Copyright
© 2022 R. Russo, B. Y. Chen
Related content
Research Group
Aerospace Structures & Computational Mechanics
Issue number
11
Volume number
123
Pages (from-to)
2676-2677
Reuse Rights

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Abstract

The authors would like to point out three writing mistakes that have been found after the publication of the original paper: Equation (13) should be written as: 1 (Formula presented.) to correctly represent the intended column vector of the element's degrees of freedom. Equation (49) and (50) should be written as: 2 (Formula presented.) to keep the vector format consistent across the terms. The derivations afterwards are not affected by this change. Equation (63) should have no minus sign on the second term of the second row, that was a typographical error. The correct Equation (63) should be written as: 4 (Formula presented.) The above mistakes appear only in the writing of the manuscript, not in the actual implementation of the method. Hence, the results and conclusions in the original paper remain unchanged. ACKNOWLEDGMENT The authors would like to thank Mr. Zhe Han from Nanjing University of Aeronautics and Astronautics for pointing out some of the above mistakes.