This　paper　investigates　nonlinear　dynamic　behaviors　of　a　rotating　blade　subjected　to　the　blast　pulse.　The　rotating　blade　is　simplified　as　a　presetting,　pretwist,　rotating　functionally　graded　material　cylindrical　panel.　According　to　the　power-law　distribution,　the　effective　material　properties　are　assumed　to　be　graded　along　the　thickness　direction.　The　centrifugal　and　Coriolis　effects　are　considered　in　the　structural　model.　Nonlinear　strain-displacement　relationships　of　the　functionally　graded　material　cylindrical　panel　are　obtained　by　the　Green　strain　tensor.　The　aerodynamic　pressure　is　derived　by　the　first-order　piston　theory.　Based　on　the　first-order　shear　deformation　theory,　nonlinear　partial　differential　governing　equations　are　obtained　by　using　the　Hamilton　principle.　Galerkin　procedure　is　used　to　acquire　the　dynamic　discrete　system.　Numerical　simulations　about　nonlinear　transient　dynamic　responses　of　the　system　subjected　to　the　blast　pulse　are　performed　by　considering　the　effects　of　different　parameters　of　the　functionally　graded　material　cylindrical　panel　©　Proceedings　of　the　26th　International　Congress　on　Sound　and　Vibration,　ICSV　2019.　All　rights　reserved.