Investigates mechanical properties of composite materials for drones, showing implications for material selection in design.
This study investigates the mechanical properties of composite materials for drone applications, focusing on Carbon Fiber Reinforced Polymer (CFRP), Glass Fiber Reinforced Polymer (GFRP), and hybrid CFRP-GFRP composites. Tensile strength, flexural strength, impact resistance, and fatigue resistance were evaluated and compared. Results show that CFRP demonstrates superior tensile and flexural strength, making it optimal for structural drone components like frames and supports. GFRP, while exhibiting lower overall strength, offers high impact resistance, rendering it suitable for non-structural parts exposed to impulse loads. Hybrid composites provide balanced performance, combining moderate strength with flexibility and cost-effectiveness. Notably, CFRP-Nano, a nano-enhanced variant, outperformed conventional CFRP across all tests, indicating significant potential for next-generation, high-demand drone applications. This research underscores the importance of material selection tailored to specific mechanical requirements in drone design and highlights the role of advanced composites in enhancing drone performance and durability.
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I et al. (2026) studied this question.
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