A unified numerical approach for the simulation of intra and inter laminar damage evolution in stiffened CFRP panels under compression-Reference-Cited by-同舟云学术

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A unified numerical approach for the simulation of intra and inter laminar damage evolution in stiffened CFRP panels under compression

Published:2020-06 Issue: Volume:190 Page:107931
ISSN:1359-8368
Container-title:Composites Part B: Engineering
language:en
Short-container-title:Composites Part B: Engineering

Author:

Kolanu Naresh Reddy,Raju Gangadharan,Ramji M

Funder

Department of Science and Technology

DST

Japan International Cooperation Agency (JICA), Japan

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference51 articles.

1. Numerical study of quasi-static and fatigue delamination growth in a post-buckled composite stiffened panel;Raimondo;Compos B Eng,2020

2. Post-buckling behaviour of flat stiffened composite panels: experiments vs. analysis;Boni;Compos Struct,2012

3. Inter-laminar and intra-laminar damage evolution in composite panels with skin-stringer debonding under compression;Raimondo;Compos B Eng,2016

4. A robust numerical approach for the simulation of skin–stringer debonding growth in stiffened composite panels under compression;Riccio;Compos B Eng,2015

5. An experimental and numerical investigation on low-velocity impact damage and compression-after-impact behavior of composite laminates;Tuo;Compos B Eng,2019

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1. A novel integrated modeling strategy for predicting damage mechanisms and energy dissipation of composite stiffened structures under low-velocity impact and compression;Aerospace Science and Technology;2024-10

2. Non-linear buckling analysis of delaminated hat-stringer panels using variational asymptotic method;Composite Structures;2024-10

3. Development and experimental verification of an advanced 3D elastoplastic progressive damage model for composite materials;Advanced Composite Materials;2024-09-02

4. Experimental and numerical studies on compressive failure behaviors of stepped-scarf repaired composite stiffened panels;Engineering Failure Analysis;2024-09

5. Optimization of composite aeronautical components by Re-designing with double-double laminates;Aerospace Science and Technology;2024-08

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