作者: Y.F. Zhang , Y. Niu , W. Zhang
DOI: 10.1016/J.ENGSTRUCT.2020.111259
关键词: Nonlinear system 、 Cantilever 、 Multiple-scale analysis 、 Hamilton's principle 、 Physics 、 Equations of motion 、 Mechanics 、 Vibration 、 Aerodynamic force 、 Galerkin method 、 Civil and Structural Engineering
摘要: Abstract This paper investigates the complex nonlinear vibrations and internal resonance of rotating blade subjected to aerodynamic force, which is simplified a pretwisted cantilever rectangular plate with varying cross-section speed. Considering effects warping, presetting angles, partial differential governing equations motion are established based on third-order shear deformation theory, von Karman large theory Hamilton principle. Two-degree-of-freedom ordinary obtained by using Galerkin method. The method multiple scales applied obtain averaged under case primary parametric resonance-1/2 subharmonic 1:2 resonance. Numerical simulations performed portray amplitude-frequency response amplitude-force curves, bifurcations chaotic dynamics discussing influences force speed perturbation. bifurcation diagrams, maximum Lyapunov exponents, phase portraits, waveforms Poincare maps utilized illustrate plate.