Aeroelastic effect on modal interaction and dynamic behavior of acoustically excited metallic panels

Aeroelastic analysis and flutter control of wings and panels: A review

“…Carrera and Zappino127 used the FEM to study the aeroelastic flutter characteristics of panels supported by a fixed number of pinched points under supersonic airflow.The influence of the number of pinched points on the critical flutter dynamic pressure was calculated. Wang et al128 studied the supersonic flutter and model interaction of acoustically excited panels with fully clamped boundary conditions using the FEM. As displayed in Figure8, Pacheco et al129 studied the nonlinear flutter characteristics of composite panels on multiple supports in high supersonic airflow using the nonlinear FEM, and multiple lamination schemes and multibay arrangements were considered.…”