Abstract

The paper is motivated by a series of wind tunnel experiments, which deal with aeroelastic Single Degree of Freedom (SDOF) and Two Degrees of Freedom (TDOF) section models. Most of them can be mathematically expressed by van der Pol-Duffing type equations or their combination. Excitation due to aeroelastic forces consists mostly of a deterministic periodic part and random components, both of them are applied as additive processes. The lock-in state represents an auto-synchronization of the vortex shedding and basic eigen-frequency of the system. This problem seems to be very polymorphous and, therefore, several isolated regimes have been outlined together with their characterization. Parameter setting with solely random excitation is further investigated in the paper. The strategy of stochastic averaging is then employed to formulate normal form of stochastic system for partial amplitudes of harmonic approximates of the response. The random part of excitation is considered as a Gaussian process with significantly variable spectral density. Hence, a conventional way of investigation based on an idea of white noise excitation is no more applicable. Therefore, the general formulation of diffuse and drift coefficients should be used to construct the relevant Fokker-Planck equation (FPE). Semi-analytical solution of FPE is deduced in the exponential form by means of a probability potential. It is later used for stochastic stability investigation together with consideration about the stationary probability distribution existence. Open problems and further research steps are outlined.

Highlights

  • The paper is motivated by a series of wind tunnel experiments investigating aeroelastic Single Degree of Freedom (SDOF) and Two Degrees of Freedom (TDOF) section models of various shape and aeroelastic properties

  • TDOF and SDOF systems have been mentioned as an integral framework

  • At the moment the SDOF system has been treated in general and in details regarding the response probability density. This basis will be used from a methodological point of view as a background of an extensive study of the general TDOF system with combined deterministic and random excitation

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Summary

Introduction

The paper is motivated by a series of wind tunnel experiments investigating aeroelastic Single Degree of Freedom (SDOF) and Two Degrees of Freedom (TDOF) section models of various shape and aeroelastic properties. (iii) V > Vcrit: vortex shedding nearly disappeared and random effects are dominating For this reason a series of consecutive papers dealing with various types of special and more general mathematical models considered as a theoretical support of aeroelastic experiments in the wind tunnel are planed. As the first step authors attempt to develop an authentic theoretical counterpart characterizing response of a nonlinear SDOF system associated with aeroelastic model, which is investigated in conditions of the homogeneous stream with the velocity slowly sweeping up and down outside the resonance domain In this regime the random excitation component of the additive type is dominant. Later stationary response using stochastic averaging will be investigated together with some parametric analyzes

Character of basic mathematical model
Fokker-Planck equation for the response partial amplitudes
System parameter θ
Conclusions
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