PERFORMANCE ANALYSIS AND STRUCTURAL OPTIMIZATION OF CARGO AIRCRAFT FIN BLADES

Abstract

The investigation investigates methods for enhancing the structural stability and performance of cargo plane fin blades to enhance their stability, effectiveness, and efficiency in utilizing airflow. The study examines the lift-to-drag ratio, stress and deformation analysis, and vibration analysis in a variety of operating circumstances. These are among the critical components that are examined. Different fin blade configurations and materials, such as lightweight composites, are examined in this paper to determine the most effective method of reducing the structure's weight while maintaining its strength. Their research demonstrates that the new designs enhance the stability of the vehicles, reduce aerodynamic drag, and achieve the highest possible petroleum mileage. Researchers have gained a greater understanding of the process of creating low-cost, high-performance fin blades. This investigation contributes to the development of cargo aircraft designs that are both robust and efficient.