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 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.
Authors
- Mathieu Préau (ORCID: https://orcid.org/0000-0002-3804-6974)
- A. Coppalle
- Jennifer Dupuis
- Benoît Vieille (ORCID: https://orcid.org/0000-0003-4528-7167)
- C Li Victor
- Thierry Le Docte
Institutions
- Normandie Université (FR)
- Groupe de Physique des Matériaux (FR)
- Safran Electronics (Canada) (CA)
- Safran (France) (FR)
- Université de Rouen Normandie (FR)
- Institut National des Sciences Appliquées Rouen Normandie (FR)
Publication Details
- Journal
- Journal of Aircraft
- Published
- 2024-12-26
- DOI
- https://doi.org/10.2514/1.c037797
- Primary Topic
- Fire dynamics and safety research
- Type
- article
- Field-Weighted Citation Impact
- 0.00