Multi-fidelity structural analysis of a beam-shaped wing
نویسندگان
چکیده
Abstract As far as integrity and proper operation of a flying vehicle are concerned, modal analysis the wing is crucial design procedure. This procedure aims to define natural frequencies structure avoid resonance under fluctuating aerodynamic loads. becomes more significant if forced perform pitching oscillation. The present study dynamic behavior rectangular with NACA 0009 airfoil using Euler-Bernoulli beam theory by treating cantilever beam. To assess validity this treatment theoretical method tool, both numerical simulations experimental measurements applied on wing. Results multi-fidelity good agreement three methods confirms in concern simple
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ژورنال
عنوان ژورنال: Journal of physics
سال: 2022
ISSN: ['0022-3700', '1747-3721', '0368-3508', '1747-3713']
DOI: https://doi.org/10.1088/1742-6596/2299/1/012009