DESIGN OF A WING SECTION AND STRUCTURAL ANALYSIS
Keywords:
CFD, wing section, airfoil, NACA, Trefftz plane method, ANSYSAbstract
This study presents the process of a wing section design and analysis of structural behavior to evaluate its aerodynamic and structural performance under real flight conditions. The conclusive design of the wing section is determined using the Trefftz plane method. This method provides essential data about critical areas of the structure, and it is used to improve structural and aerodynamic performance.
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