A modular method for helicopter blade modeling and structural load calculation based on the finite element tearing and interconnecting

Applied Mathematical Modelling 2026

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Authors: Chuanda Wang, Hao Wang, Gang Wang, Yun Zhou, Wen Zhou, Haijun Peng

DOI: 10.1016/j.apm.2026.116858

Cited by: 0

References: 29

Fields of Study & Subjects

Aeroelasticity and Vibration Control Bladed Disk Vibration Dynamics Advanced Numerical Methods in Computational Mathematics

References 29