Enhanced LaRC05 failure criteria for investigating low-velocity impact on fiber-reinforced composites: An experimental and computational study
Authors:
- Peyman ShabaniPSPeyman Shabani
- Lucy LiLLLucy Li
- Jeremy LaliberteJLJeremy Laliberte
- Gang QiGQGang Qi
Open Access
- 12 September 2024
- journal article
- research article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 155
Abstract
No abstract availableKeywords
Funding Information
- Department of National Defence and the Canadian Armed Forces
- Natural Sciences and Engineering Research Council of Canada
- Ministère de la Défense Nationale
- Alliance de recherche numérique du Canada
This publication has 70 references indexed in Scilit:
- A newly proposed damage constitutive model for composite laminates under low-velocity impact by considering through-thickness compression damageAerospace Science and Technology, 2023
- Compression after multiple impact strength of composite laminates prediction method based on machine learning approachAerospace Science and Technology, 2023
- Finite element analysis on impact response and damage mechanism of composite laminates under single and repeated low-velocity impactAerospace Science and Technology, 2022
- Repeated low-velocity impact response and damage mechanism of glass fiber aluminium laminatesAerospace Science and Technology, 2019
- A concise interface constitutive law for analysis of delamination and splitting in composite materials and its application to scaled notched tensile specimensInternational Journal for Numerical Methods in Engineering, 2006
- Formulation and implementation of decohesion elements in an explicit finite element codeComposites Part A: Applied Science and Manufacturing, 2006
- A constitutive model for anisotropic damage in fiber-compositesMechanics of Materials, 1995
- Damage mechanism characterization in composite damage tolerance investigationsComposite Structures, 1993
- A comparison of failure criteria to predict delamination of unidirectional glass/epoxy specimens waisted through the thicknessComposites, 1992
- Crack band theory for fracture of concreteMaterials and Structures, 1983