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Jia-Tai Hu

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Open access 2026

Finite element analysis of static and modal characteristics of quadrotor UAVs

Structural stiffness and low-frequency vibration characteristics govern the load-carrying reliability of a quadrotor airframe. An ANSYS Workbench finite-element model was used to calculate the response of a four-arm frame under central downward loads of 100, 200, and 300 N. Equivalent stress, total deformation, the fir...

Jia-Tai Hu · 0 citations

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