Kurtaran, Hasan2025-01-062025-01-0620181300-18841304-491510.17341/gazimmfd.4163462-s2.0-85049735568https://doi.org/10.17341/gazimmfd.416346https://search.trdizin.gov.tr/tr/yayin/detay/287978https://hdl.handle.net/20.500.14669/2758In this study, dynamic behavior of moderately thick symmetrically laminated composite cylindrical panel under moving load is investigated using Ritz solution approximations. Hamilton's principle (also referred to as dynamic version of Virtual work principle) is used to derive the equation of motion. First order shear deformation theory is used to consider transverse shear effect. Time integration of equation of motion is carried out using implicit Newmark average acceleration method. Parametric study is conducted in order to investigate the dynamic behavior of composite cylindrical panel for different velocities of moving load, curvature ratios, stacking schemes and boundary conditions.trinfo:eu-repo/semantics/openAccessMoving loadRitz methodLaminated compositeCylindrical panelFirst order shear deformation theoryArticle3912Q238128797833WOS:000435972700002Q4