Incremental harmonic balance method for nonlinear flutter of an airfoil with uncertain-but-bounded parameters
DOI10.1016/J.APM.2011.07.016zbMath1236.74071OpenAlexW2064667880MaRDI QIDQ2428917
Publication date: 21 April 2012
Published in: Applied Mathematical Modelling (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.apm.2011.07.016
Monte Carlo methods (65C05) Topological structure of integral curves, singular points, limit cycles of ordinary differential equations (34C05) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Random vibrations in dynamical problems in solid mechanics (74H50) Multifrequency systems of ordinary differential equations (34C46)
Related Items (7)
Cites Work
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- Homotopy analysis method for limit cycle flutter of airfoils
- Uncertainty quantification of limit-cycle oscillations
- The secondary bifurcation of an aeroelastic airfoil motion: effect of high harmonics
- Chebyshev polynomial approximation for dynamical response problem of random system
- Structural non-linearities and the nature of the classic flutter instability
- Amplitude Incremental Variational Principle for Nonlinear Vibration of Elastic Systems
- Bifurcation analysis of airfoils in incompressible flow
- Flutter analysis of an airfoil with bounded random parameters in incompressible flow via Gegenbauer polynomial approximation
- A modern course in aeroelasticity.
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