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Nonlinear aeroelastic stability analysis of hingeless helicopter rotor blades using FRF coupling and condition number
Authors:S. A. S. Roknizadeh  A. S. Nobari  H. Shahverdi
Affiliation:1. Department of Mechanical Engineering, Faculty of Engineering, Shahid Chamran University of Ahvaz, Ahvaz, Iran
2. Aerospace Engineering Department and Center of Excellence in Computational Aerospace, AmirKabir University of Technology, 15875-4413, Tehran, Iran
Abstract:
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