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Record W4410453608 · doi:10.18280/rcma.350214

Analytical Modeling of Delamination in T300-3000 Epoxy Carbon Fiber Composites under Three-Point Bending Test

2025· article· fr· W4410453608 on OpenAlexvenueno aff
Fatima Zohra Diar, Youssef Benbouras, Mohammed Ouabdou, Benaissa El Fahime, Mohammed Radouani

Bibliographic record

VenueRevue des composites et des matériaux avancés · 2025
Typearticle
Languagefr
FieldEngineering
TopicMechanical Behavior of Composites
Canadian institutionsnot available
FundersCentre National pour la Recherche Scientifique et Technique
KeywordsEpoxyComposite materialMaterials scienceDelamination (geology)BendingFiber pull-outThree point flexural testFiberComposite laminatesComposite number

Abstract

fetched live from OpenAlex

The use of composite materials has emerged as a critical alternative to traditional metallic structures, particularly in aerospace engineering where high strength-to-weight ratio and structural integrity are essential.This paper presents an analytical and experimental investigation of delamination in T300-3000 epoxy carbon fiber composites subjected to three-point bending tests.The main contribution lies in the development of a predictive model integrating Classical Plate Theory (CPT) with the Tsai-Hill failure criterion to assess delamination initiation and propagation.A specially designed multilayered laminate was tested under standardized conditions, and a strong correlation was observed between experimental results and model predictions, with a deviation of less than 8% in peak load estimations.The mechanical properties of the epoxy interface, along with Fiber Volume Fraction (FVF), were also taken into account for a more accurate representation of interlaminar stress distribution.The study highlights the limitations of the Tsai-Hill criterion, particularly in differentiating tensile and compressive transverse failures, and recommends the inclusion of higher-order shear deformation theories in future work.The proposed approach offers valuable insights into the structural behavior of composites under flexural loading and can guide the design of more damage-tolerant aerospace components through better laminate configuration and non-destructive evaluation strategies.

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

How this classification was reachedexpand

Full frame machine prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. The Gemma side is a direct model label for every work in the frame, read from the title-only record. The Codex side is a classifier learned from the 10,348 direct Codex labels and calibrated to design-weighted sample rates; fields without enough sample support carry no Codex call. Candidate is the union of the two sides; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels.

metaresearch head score (Codex)0.000
metaresearch head score (Gemma)0.000
Version: metacan-v3-hybrid-931329e0061cValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Simulation or modeling · Consensus signal: Simulation or modeling
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.004
Threshold uncertainty score0.008

Distilled classifier scores by category (both heads)

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0000.000
Open science0.0010.000
Research integrity0.0010.000
Insufficient payload (model declined to judge)0.0010.000

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.054
GPT teacher head0.295
Teacher spread0.241 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it

Classification

machine, unvalidated

Machine predicted; a candidate call from one source (direct Gemma or distilled Codex), not a consensus.

The models applied no category: nothing in the taxonomy fit this work.
Study designSimulation or modeling
Domainnot available
GenreEmpirical

How this classification was reached, model by model and score by score, is at the end of the page under "How this classification was reached".

Quick stats

Citations0
Published2025
Admission routes1
Has abstractyes

Explore more

Same venueRevue des composites et des matériaux avancésSame topicMechanical Behavior of CompositesFrench-language works237,207