Effect of Boundary Condition on Numerical Study of UAV Composite Skin Panels Under Dynamic Impact Loading

Effect of Boundary Condition on Numerical Study of UAV Composite Skin Panels Under Dynamic Impact Loading

In this study, a dynamic impact loading using Finite Element Analyses (FEA) was applied to an Unmanned Aerial Vehicle (UAV) composite skin panel. Two types of boundary condition panels were investigated (Fixed and Pinned). The composite UAV skin panel consists of upper panel and stiffener which have...

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Bibliographic Details
Main Authors: Ilham Bagus Wiranto, Sherly Octavia Saraswati, Iqbal Reza Alfikri, Chairunnisa Chairunnisa, Fadli Cahya Megawanto, Muhammad Ilham Adhynugraha, Nur Cholis Majid
Format: Article
Language:English
Published: Teknik mesin, Fakultas Teknik, Universitas Sebelas Maret 2024-03-01
Series:Mekanika
Online Access:https://jurnal.uns.ac.id/mekanika/article/view/77875
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https://jurnal.uns.ac.id/mekanika/article/view/77875

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