Flutter and Thermal Buckling Analysis for Composite Laminated Panel Embedded with Shape Memory Alloy Wires in Supersonic Flow

Figure 5

Flutter boundary versus position of layer embedded with SMA wires (, [60/−60/60/−60]_s;, [/−60/60/−60]_s;, [60//60/−60]_s;, [60/−60//−60]_s; , [60/−60/60/]_s.).