Design, Modeling, and Comprehensive Analysis for The Wing of an Aircraft

This study examines the design and analysis of a training aircraft wing. The methodology includes aerodynamic and stress analyses. Microsoft Excel is utilized for scaling. Aerodynamic forces, load distribution, and air foil comparison computations were performed by Xflr 5. Inventor was used for str...

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Bibliographic Details
Main Authors: Hakam Waadallah Shehab, Mohammed Saleh Mohammed, Mohammed Najeeb Abdullah
Format: Article
Language:English
Published: Northern Technical University 2025-03-01
Series:NTU Journal of Engineering and Technology
Subjects:
Online Access:https://journals.ntu.edu.iq/index.php/NTU-JET/article/view/1202
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