A Poisson-Process Model for Cumulative Delamination Damage in Composite Materials

ABSTRACT This study presents a probabilistic model for cumulative damage in composite materials undergoing delamination. The model assumes the presence of numerous weak microvolumes (WMVs) in which fatigue damage can initiate and accumulate. Defect nucleation is described as a Poisson process whose rate does not depend on specimen size. The cumulative distribution function of the fatigue life of each microvolume is obtained using the Poisson formulation, and the overall delamination behavior is interpreted as a brittle-type failure mechanism governed by nodal attachment points in honeycomb structures. Numerical implementation is demonstrated through Excel-based inverse comparison and R-based simulation methods. The results show that Poisson-driven damage evolution provides a viable approach for estimating residual undamaged area and for modelling avalanche-type delamination growth. The methodology offers a foundation for future experimental verification and refinement of stochastic models for composite damage propagation.

Authors

Institutions

Publication Details

Journal
Transactions of the Institute of Aviation
Published
2025-12-01
DOI
https://doi.org/10.2478/tar-2025-0022
Primary Topic
Mechanical Behavior of Composites
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

A Poisson-Process Model for Cumulative Delamination Damage in Composite Materials

Rafał. Oprac. Chatys, Konstantin N. Nechval
Transactions of the Institute of Aviation
Mechanical Behavior of Composites
article

A Poisson-Process Model for Cumulative Delamination Damage in Composite Materials

Rafał. Oprac. Chatys, Konstantin N. Nechval
article en

Abstract

ABSTRACT This study presents a probabilistic model for cumulative damage in composite materials undergoing delamination. The model assumes the presence of numerous weak microvolumes (WMVs) in which fatigue damage can initiate and accumulate. Defect nucleation is described as a Poisson process whose rate does not depend on specimen size. The cumulative distribution function of the fatigue life of each microvolume is obtained using the Poisson formulation, and the overall delamination behavior is interpreted as a brittle-type failure mechanism governed by nodal attachment points in honeycomb structures. Numerical implementation is demonstrated through Excel-based inverse comparison and R-based simulation methods. The results show that Poisson-driven damage evolution provides a viable approach for estimating residual undamaged area and for modelling avalanche-type delamination growth. The methodology offers a foundation for future experimental verification and refinement of stochastic models for composite damage propagation.

Transactions of the Institute of AviationVol. 2025(4)
Kielce University of Technology (PL), Riga Aeronautical Institute (LV)
Openalex Percentile: Top 40%
Mechanical Behavior of Composites
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.

A Poisson-Process Model for Cumulative Delamination Damage in Composite Materials — Rafał. Oprac. Chatys, Konstantin N. Nechval · Transactions of the Institute of Aviation (2025) | TGRS Research Map | TGRS