... of aerospace-grade laminated composite panels under dynamic loading. Design/methodology/approach T-stiffened composite panels were simulated in LS-DYNA under a 1.5 kg, 7.5 m/s low-velocity impact. The Taguchi L₉ method evaluated the effects of layer number, thickness and stacking sequence...

...-based computer code developed in MATLAB environment. Subsequently, a simulation model has been developed in ANSYS using ANSYS parametric design language code to evaluate the responses. Findings – Vibration and thermal buckling responses of laminated composite curved panels have been obtained based...