Fire Reaction of Carbon Epoxy Composite Laminates at Small and Large Scales
To study the antiflammability of composite material panels, assemblies, or components, certification standards require significant [Formula: see text] samples to withstand a kerosene flame for 15-min tests. To better analyze thermophysical phenomena involved in a flame exposition of composite-based...
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Veröffentlicht in: | Journal of aircraft 2024-12, p.1-9 |
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Hauptverfasser: | , , , , , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | To study the antiflammability of composite material panels, assemblies, or components, certification standards require significant [Formula: see text] samples to withstand a kerosene flame for 15-min tests. To better analyze thermophysical phenomena involved in a flame exposition of composite-based samples, a laboratory test bench composed of a small-scale air–kerosene burner has been developed. The current work presents the development of a representative kerosene burner in terms of aerothermal stress generated by determining the right settings for the flame parameters and by comparing the fire-induced degradation process of several four-ply epoxy-composite samples. Two laboratory-scale tests are made and compared to a large-scale one made on a standardized fire test bench. |
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ISSN: | 0021-8669 1533-3868 |
DOI: | 10.2514/1.C037797 |