作者: I. H. Choi , C. S. Hong
DOI: 10.2514/3.12253
关键词: Structural engineering 、 Composite laminates 、 Contact mechanics 、 Materials science 、 Isotropy 、 Material properties 、 Impact 、 Finite element method 、 Orthotropic material 、 Modal analysis 、 Aerospace engineering
摘要: A new method for simple prediction of the impact force history on composite laminates subjected to low-velocity is proposed. First, calculated from response analysis using finite element incorporated with modified Hertzian contact law. Frequency characteristics numerical are investigated modal and compared natural frequencies system in which mass an impactor lumped plate. The present can be efficiently applied isotropic or orthotropic plates unknown laws as well no restraint material properties geometrical shape