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Critical review of interlaminar damage process and failure analysis in fiber-reinforced composite laminates encompassing fiber-bridging phenomenon

Identifikátory výsledku

  • Kód výsledku v IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24210%2F25%3A00013151" target="_blank" >RIV/46747885:24210/25:00013151 - isvavai.cz</a>

  • Nalezeny alternativní kódy

    RIV/46747885:24620/25:00013151

  • Výsledek na webu

    <a href="https://journals.sagepub.com/doi/epdf/10.1177/00219983251313669?src=getftr&utm_source=scopus&getft_integrator=scopus" target="_blank" >https://journals.sagepub.com/doi/epdf/10.1177/00219983251313669?src=getftr&utm_source=scopus&getft_integrator=scopus</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1177/00219983251313669" target="_blank" >10.1177/00219983251313669</a>

Alternativní jazyky

  • Jazyk výsledku

    angličtina

  • Název v původním jazyce

    Critical review of interlaminar damage process and failure analysis in fiber-reinforced composite laminates encompassing fiber-bridging phenomenon

  • Popis výsledku v původním jazyce

    Metallic structures are increasingly being replaced by fiber-reinforced composites for the design of advanced structures with superior mechanical and physical properties. Fibrous composites offer several advantages, including lightweight feature while maintaining mechanical strength, resistance to damage evolution, and high fracture tolerance. Delamination growth in laminated composites is sometimes accompanied by fiber bridging which provides additional resistance against delamination growth. Delamination is known as one of the primary causes of premature failure in laminated composites. It is therefore necessary to gain a comprehensive understanding of interlaminar damage. Much research has been done to study various characteristics of fiber bridging yet the challenge remains an open topic for continued research. This review article aims to report the major studies on fiber bridging of composite materials in the literature. This article starts with an introduction to various modes of failure observed in fiber-reinforced laminated composites, extrinsic and intrinsic damage mechanisms, and the delamination phenomenon in the presence of fiber bridging. Next, different experimental and numerical methods for the characterization of delamination are presented. Fatigue-driven delamination, a leading cause of failure in aerospace structures, is subsequently reviewed. The paper concludes with a review of practical applications of numerical methods for delamination analysis followed by a review of recent progress in this field as well as open challenges in modeling, simulation, and experimental research works on the mechanics of fiber bridging incorporating composite damage and failure.

  • Název v anglickém jazyce

    Critical review of interlaminar damage process and failure analysis in fiber-reinforced composite laminates encompassing fiber-bridging phenomenon

  • Popis výsledku anglicky

    Metallic structures are increasingly being replaced by fiber-reinforced composites for the design of advanced structures with superior mechanical and physical properties. Fibrous composites offer several advantages, including lightweight feature while maintaining mechanical strength, resistance to damage evolution, and high fracture tolerance. Delamination growth in laminated composites is sometimes accompanied by fiber bridging which provides additional resistance against delamination growth. Delamination is known as one of the primary causes of premature failure in laminated composites. It is therefore necessary to gain a comprehensive understanding of interlaminar damage. Much research has been done to study various characteristics of fiber bridging yet the challenge remains an open topic for continued research. This review article aims to report the major studies on fiber bridging of composite materials in the literature. This article starts with an introduction to various modes of failure observed in fiber-reinforced laminated composites, extrinsic and intrinsic damage mechanisms, and the delamination phenomenon in the presence of fiber bridging. Next, different experimental and numerical methods for the characterization of delamination are presented. Fatigue-driven delamination, a leading cause of failure in aerospace structures, is subsequently reviewed. The paper concludes with a review of practical applications of numerical methods for delamination analysis followed by a review of recent progress in this field as well as open challenges in modeling, simulation, and experimental research works on the mechanics of fiber bridging incorporating composite damage and failure.

Klasifikace

  • Druh

    J<sub>imp</sub> - Článek v periodiku v databázi Web of Science

  • CEP obor

  • OECD FORD obor

    20505 - Composites (including laminates, reinforced plastics, cermets, combined natural and synthetic fibre fabrics; filled composites)

Návaznosti výsledku

  • Projekt

    <a href="/cs/project/EF16_025%2F0007293" target="_blank" >EF16_025/0007293: Modulární platforma pro autonomní podvozky specializovaných elektrovozidel pro dopravu nákladu a zařízení</a><br>

  • Návaznosti

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Ostatní

  • Rok uplatnění

    2025

  • Kód důvěrnosti údajů

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Údaje specifické pro druh výsledku

  • Název periodika

    Journal of Composite Materials>

  • ISSN

    0021-9983

  • e-ISSN

  • Svazek periodika

    59

  • Číslo periodika v rámci svazku

    12

  • Stát vydavatele periodika

    GB - Spojené království Velké Británie a Severního Irska

  • Počet stran výsledku

    39

  • Strana od-do

    1553-1591

  • Kód UT WoS článku

    001399751600001

  • EID výsledku v databázi Scopus

    2-s2.0-85215627894