Sayman O.Akbulut H.Meriç C.2024-07-222024-07-22200000457949http://akademikarsiv.cbu.edu.tr:4000/handle/123456789/20495The study presents an elasto-plastic stress analysis of symmetric and antisymmetric cross-ply, angle-ply laminated metal-matrix composite plates. Long stainless steel fiber reinforced aluminum metal-matrix composite layer is manufactured by using moulds under the action of 30 MPa pressure and heating up to 600 °C. A laminated plate consists of four metal-matrix layers bonded symmetrically or antisymmetrically. The first-order shear deformation theory and nine-node Lagrangian finite element is used. The in-plane load is increased gradually.EnglishAluminumElastoplasticityFiber reinforced metalsFinite element methodLaminated compositesPlates (structural components)Pressure effectsShear deformationStainless steelStress analysisStructural analysisThermal effectsIn plane loadingLaminated platesMetallic matrix compositesArticle10.1016/S0045-7949(99)00086-3