2021
DOI: 10.1016/j.compositesa.2021.106515
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On the source of the thermoelastic response from orthotropic fibre reinforced composite laminates

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Cited by 17 publications
(3 citation statements)
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“…The heat was applied to the laminate's top surface and is distributed from the top layer (layer 1) to the bottom layer (layer 4) with the Stefan-Boltzmann constant = 5.67 x 10-8 Wm −2 K −4 and emissivity ϵ = 0.96. 12 Furthermore, the sample orientation was aligned with the global axis, which identifies the different faces of the laminate. The specimen model and its boundary conditions for the thermal loading are presented in Figure 1.…”
Section: Thermal Stepmentioning
confidence: 99%
“…The heat was applied to the laminate's top surface and is distributed from the top layer (layer 1) to the bottom layer (layer 4) with the Stefan-Boltzmann constant = 5.67 x 10-8 Wm −2 K −4 and emissivity ϵ = 0.96. 12 Furthermore, the sample orientation was aligned with the global axis, which identifies the different faces of the laminate. The specimen model and its boundary conditions for the thermal loading are presented in Figure 1.…”
Section: Thermal Stepmentioning
confidence: 99%
“…Both the load and temperature signals are post processed to using a 'lock-in' procedure to provide a temperature change, ∆T, which is directly proportional to the stress change. Typically, TSA provides surface data but can detect damage (for example cracks) at various depths depending on the loading frequency and associated level of thermal response, recently demonstrated by Jiménez-Fortunato et al [63].…”
Section: Thermographymentioning
confidence: 99%
“…The boundary conditions assigned to the sample model are determined by how it interacts with the external surroundings to accurately represent the physical phenomena of the experimental set-up which may insulate the edges. The heat was applied at the top surface of the laminate and is distributed from the top layer (layer 1) towards the bottom (layer 6) with the Stefan-Boltzmann constant = 5.67 × 10 −8 Wm −2 K −4 and emissivity = 0.96 [42]. In addition, the sample orientation was positioned correspondingly with the global axis, which identifies the different faces of the laminate.…”
Section: Boundary Problem Formulationmentioning
confidence: 99%