Effect of structural parameters on the synchronization characteristics in a stall-induced aeroelastic system
Dheeraj Tripathi, Chandan Bose, Sirshendu Mondal, J Venkatramani

TL;DR
This paper investigates how structural parameters influence bifurcation and synchronization mechanisms in a nonlinear stall-induced aeroelastic system through wind tunnel experiments with an airfoil.
Contribution
It is the first study to systematically analyze the impact of multiple structural parameters on stall-induced instabilities using synchronization analysis.
Findings
Identification of bifurcation routes under various structural parameters
Demonstration of modal interactions influencing instabilities
Documentation of the role of synchronization in aeroelastic transitions
Abstract
This study focuses on discerning the role of structural parameters on the bifurcation characteristics and the underlying synchronization mechanism in an aeroelastic system undergoing nonlinear stall behaviour. To that end, wind tunnel experiments are performed on a NACA 0012 airfoil capable of undergoing bending (plunging) and torsional (pitching) oscillations under scenarios involving nonlinear aerodynamic loads, i.e., dynamic stall conditions. Flow conditions under both deterministic/sterile flows and fluctuating/stochastic flows are fostered. The structure possesses continuous or polynomial-type stiffness nonlinearities, and therefore, is an aeroelastic experiment involving both structural and aerodynamic nonlinearities. We discern the bifurcation routes for a range of key structural parameters such as frequency ratio, static imbalance, and the extent of structural nonlinearity. In…
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Taxonomy
TopicsFluid Dynamics and Vibration Analysis · Aerodynamics and Fluid Dynamics Research · Vibration and Dynamic Analysis
