With the increased use of composites in aircraft, many new successful contributions to the
advancement of the structural health monitoring (SHM) field for composite aerospace …

A health indicator (HI) is a valuable index demonstrating the health level of an engineering
system or structure, which is a direct intermediate connection between raw signals collected …

We present a generic methodology for developing a Health Indicator out of strain-based
Structural Health Monitoring data suitable for implementation in prognostic tasks. For this …

In this study, a multi-level Structural Health Monitoring methodology for stiffened composite
panels is introduced. A digital twin (DT), that is, a three-dimensional finite element (FE) …

Damage prognosis generally resorts to damage quantification functions and evolution
models to quantify the current damage state and to predict the future states and the …

The development of numerical methodologies to investigate material damages is a crucial
aspect of aerospace components design. The advent of composite materials has made this …

Axial compressive performances of stiffened composite panel were studied in this
manuscript. In experimental study, buckling phenomenon of three specimens appear at …

Fiber reinforced polymer (FRP) structures may experience cumulative fatigue damage
during their service life which can lead to structural failure. This paper focuses on predicting …

Developing comprehensive health indicators (HIs) for composite structures encompassing
various damage types is challenging due to the stochastic nature of damage accumulation …

Fatigue damage prognosis studies typically involve updating a degradation model based on
the collected measurements. The updated model can accurately depict the past degradation …