Corrigendum to “Scaling effects of composite laminates under out-of-plane loading” [Composites Part A 116 (2019) 1–12](S1359835X18303907)(10.1016/j.compositesa.2018.10.001)

A. Wagih; P. Maimí; N. Blanco; E. V. González

doi:10.1016/j.compositesa.2019.02.005

Corrigendum to “Scaling effects of composite laminates under out-of-plane loading” [Composites Part A 116 (2019) 1–12](S1359835X18303907)(10.1016/j.compositesa.2018.10.001)

A. Wagih, P. Maimí, N. Blanco, E. V. González

Research output: Contribution to journal › Article › peer-review

Abstract

Corrections: Eq. (10) in page 3 was written incorrectly during the proof reading of the article which lead to incorrect prediction of delamination area in its current form. The Macauley brackets were missing. However, the prediction presented in the paper is obtained using the correct formula as follow: [Formula presented]where are the Macauley brackets. According to this, the delamination area increases proportionally to the displacement with a slope of [Formula presented].

Original language	English (US)
Journal	Composites Part A: Applied Science and Manufacturing
Volume	119
DOIs	https://doi.org/10.1016/j.compositesa.2019.02.005
State	Published - Apr 1 2019
Externally published	Yes

ASJC Scopus subject areas

Mechanics of Materials
Ceramics and Composites

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10.1016/j.compositesa.2019.02.005

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title = "Corrigendum to “Scaling effects of composite laminates under out-of-plane loading” [Composites Part A 116 (2019) 1–12](S1359835X18303907)(10.1016/j.compositesa.2018.10.001)",

abstract = "Corrections: Eq. (10) in page 3 was written incorrectly during the proof reading of the article which lead to incorrect prediction of delamination area in its current form. The Macauley brackets were missing. However, the prediction presented in the paper is obtained using the correct formula as follow: [Formula presented]where are the Macauley brackets. According to this, the delamination area increases proportionally to the displacement with a slope of [Formula presented].",

author = "A. Wagih and P. Maim{\'i} and N. Blanco and Gonz{\'a}lez, {E. V.}",

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language = "English (US)",

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journal = "Composites Part A: Applied Science and Manufacturing",

issn = "1359-835X",

publisher = "Elsevier Ltd",

}

Corrigendum to “Scaling effects of composite laminates under out-of-plane loading” [Composites Part A 116 (2019) 1–12](S1359835X18303907)(10.1016/j.compositesa.2018.10.001). / Wagih, A.; Maimí, P.; Blanco, N. et al.
In: Composites Part A: Applied Science and Manufacturing, Vol. 119, 01.04.2019.

Research output: Contribution to journal › Article › peer-review

TY - JOUR

T1 - Corrigendum to “Scaling effects of composite laminates under out-of-plane loading” [Composites Part A 116 (2019) 1–12](S1359835X18303907)(10.1016/j.compositesa.2018.10.001)

AU - Wagih, A.

AU - Maimí, P.

AU - Blanco, N.

AU - González, E. V.

N1 - Generated from Scopus record by KAUST IRTS on 2023-09-21

PY - 2019/4/1

Y1 - 2019/4/1

N2 - Corrections: Eq. (10) in page 3 was written incorrectly during the proof reading of the article which lead to incorrect prediction of delamination area in its current form. The Macauley brackets were missing. However, the prediction presented in the paper is obtained using the correct formula as follow: [Formula presented]where are the Macauley brackets. According to this, the delamination area increases proportionally to the displacement with a slope of [Formula presented].

AB - Corrections: Eq. (10) in page 3 was written incorrectly during the proof reading of the article which lead to incorrect prediction of delamination area in its current form. The Macauley brackets were missing. However, the prediction presented in the paper is obtained using the correct formula as follow: [Formula presented]where are the Macauley brackets. According to this, the delamination area increases proportionally to the displacement with a slope of [Formula presented].

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DO - 10.1016/j.compositesa.2019.02.005

M3 - Article

SN - 1359-835X

VL - 119

JO - Composites Part A: Applied Science and Manufacturing

JF - Composites Part A: Applied Science and Manufacturing

ER -

Corrigendum to “Scaling effects of composite laminates under out-of-plane loading” [Composites Part A 116 (2019) 1–12](S1359835X18303907)(10.1016/j.compositesa.2018.10.001)

Abstract

ASJC Scopus subject areas

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