AbstractRecent wind tunnel studies have shown that an aeroelastic system, prior to losing stability through flutter, goes through a regime where the response is characterized by intermittent bursts of periodic oscillations. The focus of this study is to investigate the reasons for this intermittent behavior through a numerical model. The studies indicate that the intermittency is observed only when the flow is accompanied by small random fluctuations. A stochastic bifurcation analysis is carried out to gain an understanding for this phenomenological interesting behavior
Stall flutter is a Limit Cycle Oscillation (LCO) caused by the periodic separation of the flow aroun...
This work presents the analysis of nonlinear aeroelastic time series from wing vibrations due to air...
The main objective of this thesis is to investigate the effects of turbulent flow on the random dyna...
Aeroelastic systems with freeplay nonlinearity can exhibit a wide variety of qualitatively different...
The interaction of an elastic structure such as an airfoil and fluid flow can give rise to nonlinear...
This paper investigates the effect of model uncertainty on the nonlinear dynamics of a generic aeroe...
The aeroelastic response of a NACA 0012 airfoil in the flow regimes prior to flutter is investigated...
Recent computational studies based on numerical solutions of the unsteady Euler equations have revea...
AbstractElastic structures like thin plates oscillating in fluid flow are susceptible to instabiliti...
The present paper investigates the effects of noisy flow fluctuations on the fluid-structure interac...
Stall flutter is a nonlinear aeroelastic phenomenon that can affect several types of aeroelastic sys...
We investigate a typical aerofoil section under dynamic stall conditions, the structural model is li...
Stall flutter is a nonlinear aeroelastic phenomenon that can affect several types of aeroelastic sys...
Flutter is usually predicted using linearised theory. In reality, flutter is always non-linear and m...
The aeroelastic behaviour of a wing oscillating in the heave and pitch degrees of freedom is examine...
Stall flutter is a Limit Cycle Oscillation (LCO) caused by the periodic separation of the flow aroun...
This work presents the analysis of nonlinear aeroelastic time series from wing vibrations due to air...
The main objective of this thesis is to investigate the effects of turbulent flow on the random dyna...
Aeroelastic systems with freeplay nonlinearity can exhibit a wide variety of qualitatively different...
The interaction of an elastic structure such as an airfoil and fluid flow can give rise to nonlinear...
This paper investigates the effect of model uncertainty on the nonlinear dynamics of a generic aeroe...
The aeroelastic response of a NACA 0012 airfoil in the flow regimes prior to flutter is investigated...
Recent computational studies based on numerical solutions of the unsteady Euler equations have revea...
AbstractElastic structures like thin plates oscillating in fluid flow are susceptible to instabiliti...
The present paper investigates the effects of noisy flow fluctuations on the fluid-structure interac...
Stall flutter is a nonlinear aeroelastic phenomenon that can affect several types of aeroelastic sys...
We investigate a typical aerofoil section under dynamic stall conditions, the structural model is li...
Stall flutter is a nonlinear aeroelastic phenomenon that can affect several types of aeroelastic sys...
Flutter is usually predicted using linearised theory. In reality, flutter is always non-linear and m...
The aeroelastic behaviour of a wing oscillating in the heave and pitch degrees of freedom is examine...
Stall flutter is a Limit Cycle Oscillation (LCO) caused by the periodic separation of the flow aroun...
This work presents the analysis of nonlinear aeroelastic time series from wing vibrations due to air...
The main objective of this thesis is to investigate the effects of turbulent flow on the random dyna...