Sensitivity Analysis of Unmanned Aerial Vehicle Composite Wing Structural Model Regarding Material Properties and Laminate Configuration

Sensitivity Analysis of Unmanned Aerial Vehicle Composite Wing Structural Model Regarding Material Properties and Laminate Configuration

This study optimizes the structural design of a composite wing shell by minimizing mass and maximizing the first natural frequency. The analysis focuses on the effects of polyvinyl chloride (PVC) foam thickness and the fiber orientation angle of the inner carbon layers, with the outer layers fixed a...

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Bibliographic Details
Main Authors: Artur Kierzkowski, Jakub Wróbel, Maciej Milewski, Angelos Filippatos
Format: Article
Language:English
Published: MDPI AG 2025-01-01
Series:Drones
Subjects:
unmanned aerial vehicle (UAV)
composite structures
Design of Experiment
response surface methodology
vibration
Online Access:https://www.mdpi.com/2504-446X/9/2/99
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