Abstract

The contribution regards a mathematical single-degree-of-freedom model of a slender structure vibrating in an air flow. Based on an experimental investigation, movement of such structures can be expressed by van der PolDuffing-type equations. Several particular configuration parameter settings for a white and non-white Gaussian random excitation together with deterministic harmonic forcing are considered and numerically analysed. The results support recently published analytic formulas.

Highlights

  • Movement of slender structures vibrating in an air flow can be modelled by van der Pol-Duffing-type equations

  • It is worthwhile to note that the character of the random excitation enters the theoretical formulas Eqs. (4,5) only through the value S, which corresponds to the value of the corresponding power spectral density at a single frequency

  • The approximative numerical stochastic analysis of a non-linear single-degree-of-freedom model was presented as a complement of previously published analytical formulas

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Summary

Introduction

Movement of slender structures vibrating in an air flow can be modelled by van der Pol-Duffing-type equations. The vortex shedding, which appears behind the structure, may induce a regular excitation, turbulence generated by an air circumfluence around the profile and its surface irregularities may cause random fluctuations of pressure. For the case of a combination of harmonic/random excitation is taken into account, the analytic formula was derived to distinguish two distinct phase shifted components of the response. This information is unavailable in the numerical results, in such a case only approximative comparison is presented.

Mathematical model
CA exp
Numerical simulation
Simulation results
Conclusions
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