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].
UR - https://linkinghub.elsevier.com/retrieve/pii/S1359835X19300466
UR - http://www.scopus.com/inward/record.url?scp=85061244299&partnerID=8YFLogxK
U2 - 10.1016/j.compositesa.2019.02.005
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 -