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

Table 1

Critical buckling temperature of the isotropic panel.

	Zhao et al. [19]	Shiau et al. [20]	Shi et al. [21]	Present
(°C)	126.5	127.1	126.4	126.43