Homotopy Analysis Method for Limit Cycle Oscillations of an Airfoil with Cubic Nonlinearities

DOI10.1177/1077546308097268zbMath1269.70039OpenAlexW1996915676MaRDI QIDQ5327538

No author found.

Publication date: 8 August 2013

Published in: Journal of Vibration and Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1177/1077546308097268

zbMATH Keywords

limit cycle oscillationnonlinear aeroelastic systemhomotopy analysis methodairfoil

Mathematics Subject Classification ID

General perturbation schemes for nonlinear problems in mechanics (70K60) Phase plane analysis, limit cycles for nonlinear problems in mechanics (70K05)

Related Items (5)

Dynamic analysis of two-degree-of-freedom airfoil with freeplay and cubic nonlinearities in supersonic flow ⋮ A new semi-analytical approach for quasi-periodic vibrations of nonlinear systems ⋮ Bifurcation analysis of aeroelastic systems with hysteresis by incremental harmonic balance method ⋮ Nonlinear output feedback control of a flexible link using adaptive neural network: stability analysis ⋮ Nonlinear output feedback control of a flexible link using adaptive neural network: controller design

Cites Work

• Unnamed Item
• An analytic approximate approach for free oscillations of self-excited systems
• The secondary bifurcation of an aeroelastic airfoil motion: effect of high harmonics
• APPLICATION OF THE CENTRE MANIFOLD THEORY IN NON-LINEAR AEROELASTICITY
• Bifurcation analysis of airfoils in incompressible flow
• Beyond Perturbation

This page was built for publication: Homotopy Analysis Method for Limit Cycle Oscillations of an Airfoil with Cubic Nonlinearities