Acceso abierto

Patterns of Acoustic Emission Changes with Alterations in the Damage Area of a Composite Material According to the Mises Criterion

Sergii Filonenko

Sergii Filonenko

Department of Computerized Electrical Systems and Technologies, National Aviation UniversityKyiv, Ukraine
Buscar este autor en
Sciendo|Google Scholar
Filonenko, Sergii
 y 
Anzhelika Stakhova

Anzhelika Stakhova

Department of Structural Mechanics, Slovak University of Technology in BratislavaBratislava, Slovakia
Buscar este autor en
Sciendo|Google Scholar
Stakhova, Anzhelika
  
26 jun 2025
Patterns of Acoustic Emission Changes with Alterations in the Damage Area of a Composite Material According to the Mises Criterion's Cover Image
Acerca de este artículo
Artículo anterior
Artículo siguiente
Cite
Descargar portada
Publicado en línea: 26 jun 2025
Páginas: 50 - 58
Recibido: 02 ago 2024
Aceptado: 01 dic 2024
DOI: https://doi.org/10.14313/jamris-2025-014
Palabras clave
© 2025 Sergii Filonenko et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Figure 1.

Dependence in the variation of equivalent stress over time, according to expression (1), during the failure of CM based on the Mises criterion. The deformation rate is set to α˜=20
Dependence in the variation of equivalent stress over time, according to expression (1), during the failure of CM based on the Mises criterion. The deformation rate is set to α˜=20

Figure 2.

Graphs of the variation in AE signal amplitudes over time in relative units during the failure of CM under transverse force, based on the Mises criterion, with varying numbers of CM elements. Simulation parameter values: v˜0=100000 ; α˜=20 ; r˜=10000 ;t˜0=0.0001 . Number of CM elements: 1 − N0; 2 − 2 · N0; 3 − 3 · N0; 4 − 4 · N0; 5 − 5 · N0
Graphs of the variation in AE signal amplitudes over time in relative units during the failure of CM under transverse force, based on the Mises criterion, with varying numbers of CM elements. Simulation parameter values: v˜0=100000 ; α˜=20 ; r˜=10000 ;t˜0=0.0001 . Number of CM elements: 1 − N0; 2 − 2 · N0; 3 − 3 · N0; 4 − 4 · N0; 5 − 5 · N0

Figure 3.

Dependencies of the maximum amplitude of the AE signal (a) and the duration of the AE signal (b) on the increasing damage area (number of elements) in CM under transverse force, based on the Mises criterion
Dependencies of the maximum amplitude of the AE signal (a) and the duration of the AE signal (b) on the increasing damage area (number of elements) in CM under transverse force, based on the Mises criterion

Figure 4.

Dependence of the area under the AE signal curve on increasing damage area (number of elements) in CM under transverse force based on the Mises criterion
Dependence of the area under the AE signal curve on increasing damage area (number of elements) in CM under transverse force based on the Mises criterion

Figure 5.

Dependencies of the percentage increase in maximum amplitude (1), area under the signal curve (2), and duration (3) of the AE signal on the increasing number of elements (damage area) in CM
Dependencies of the percentage increase in maximum amplitude (1), area under the signal curve (2), and duration (3) of the AE signal on the increasing number of elements (damage area) in CM
Idioma:
Inglés
Calendario de la edición:
4 veces al año
Temas de la revista:
Informática, Inteligencia artificial, Ingeniería, Ingeniería eléctrica, Ingeniería de Control, metrología y ensayos, Ingeniería mecánica, Fundamentos de ingeniería mecánica
RSS Feed de revista