Discrete element approach to flutter of skew panels with in-plane forces under yawed supersonic flow

Aeroelastic Analysis of Composite Pinched Panels Using Higher-Order Shell Elements

“…The effects of thermal [9] and inplane [10] loads can be considered as well as the use of anisotropic, layered and composite materials as shown in the works by Shiau and Lu [11], Dixon and Mei [12], and Kouchakzadeh et al [13]. The use of advanced aerodynamic models allows the analysis to be extended to larger Mach number regimes, as shown by Gordiner and Visbal [14] and Hashimoto et al [15].…”