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What is Aircraft Wing Modal Analysis for SAE Competition about?

This conference paper presents a numerical modal analysis of an aircraft wing prototype designed for the SAE Aerodesign competition, focusing on optimizing structural efficiency while ensuring safety through the understanding of modal parameters. The study employs finite element modeling to analyze the wing structure and compares numerical results with experimental data, achieving an average difference of 5.8% in natural frequencies. The findings emphasize the importance of modal analysis in the design proc

Author

sssiddharthsharma001

Language

EN