مشروع البحث: AERODYNAMIC OPTIMIZATION OF UAV WING DESIGN USING COMPUTATIONAL FLUID DYNAMICS (CFD) ANALYSIS
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المساهمين
الممولين
رقم التعريف
817
الباحث
Ezar Shaban A DHAN
الوصف
The results demonstrated that Epoxy SMC offered superior stiffness and experienced the least deformation under load, making it an optimal choice for applications where minimizing structural displacement is critical. On the other hand, Epoxy E-glass excelled in terms of safety, with the highest safety factor, ensuring that the structure can reliably endure extreme operational conditions. Although aluminum, the traditional material, performed adequately, it did not surpass the composite materials in any significant category.
These findings underscore the potential benefits of utilizing composite materials over aluminum, particularly in UAV applications that demand structural efficiency, reduced weight, and improved safety. Epoxy SMC emerged as the best material for reducing displacement and strain on the wing, while Epoxy E-glass proved to be the safest and most reliable option. This provides valuable direction for future UAV designs, highlighting the advantages of advanced composite materials in enhancing both aerodynamic and structural performance.
الكلمات الدالة
AERODYNAMIC OPTIMIZATION OF UAV WING