研究目的
Investigating the effects of a piezoelectric based nonlinear energy sink (NES) on the aeroelastic behavior of an electromechanically coupled 2-DOF typical section for flutter suppression.
研究成果
The piezoelectric based NES effectively suppresses flutter oscillations and increases the flutter boundary by 18.4%. It demonstrates robustness against detuning and enables one-way energy transfer from mechanical to electrical domain.
研究不足
The study is limited by the maximum inductance value and voltage across the piezoelectric material, which may restrict the range of parameters that can be effectively analyzed.
1:Experimental Design and Method Selection:
The study employs an equivalent electrical circuit model to simulate the electromechanically coupled typical section with a nonlinear shunt circuit.
2:Sample Selection and Data Sources:
The properties of the piezoaeroelastic typical section are used, including parameters like airflow speed, initial plunge displacement, and piezoelectric material properties.
3:List of Experimental Equipment and Materials:
Piezoceramics (QP10n from Mide Corp.) are used with specific capacitance and electromechanical coupling parameters.
4:Experimental Procedures and Operational Workflow:
Simulations are conducted with varying NES parameters to analyze their effects on system behavior.
5:Data Analysis Methods:
The performance is evaluated based on time responses of pitch and plunge DOFs, energy analysis, and robustness against detuning.
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