In order to control the flutter of panels in supersonic flow, piezoelectric patches were bonded to the panel surfaces where flutter deformations were large.Each piezoelectric patch was connected with a negative capacitance shunt, which was utilized to modify the bending rigidity of the panel so as to boost the flutter critical speed.The results of finite element calculations demonstrate that the modal frequencies and flutter critical speed of the panel were effectively enhanced by attaching negative capacitance shunts.With increasing the magnitude of negative capacitance , especially when it approaches to the inherent capacitance of the piezoelectric patch, the flutter critical speed of the panel increases rapidly.The results of nonlinear flutter calculations also validate the effectiveness of the negative capacitance shunts control.
陈圣兵,吴东升,王锋,武龙. 超声速气流中壁板颤振分析及负电容分流控制[J]. 振动与冲击, 2020, 39(22): 23-27.
CHEN Shengbing,WU Dongsheng,WANG Feng,WU Long. Analysis and control of panel flutter in supersonic flow by attaching negative capacitance shunts. JOURNAL OF VIBRATION AND SHOCK, 2020, 39(22): 23-27.
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