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Parametric CAD Modelling of Aircraft Wings for FEA Vibration Analysis
2021
Journal of Applied Mathematics and Physics
Excessive vibration of aircraft wings during flight is harmful and may cause propagation of existing cracks in the material, leading to catastrophic failures as a result of material fatigue. This study investigates the variations of modal characteristics of aircraft wings with respect to changes in the structural configurations. We develop parametric Computer-Aided Design (CAD) models to capture new design intend on the aircraft wing architectures. Subsequent Finite Element Analysis (FEA) based
doi:10.4236/jamp.2021.95060
fatcat:birwesjpfzdarab6ehqepe4efq