Geometry > kg_QuadPlate
kg_QuadPlate
Purpose
geometric stiffness matrix for quadrilateral plate element for different options
Synopsis
kg = kg_QuadPlate (option,xyz,u,pl)
Description
KG_QUADPLATE geometric stiffness matrix for quadrilateral plate element for different options KG = KG_QUADPLATE (OPTION,XYZ,U,PL); the function determines the geometric stiffness matrix KG of a quad plate element with end coordinates in array XYZ (columns correspond to nodes); the geometric stiffness matrix depends on the node displacement values in array U (ndm x nen) in the global reference system and on the local nodal force vector PL; (nen = number of nodes) OPTION is a character variable with value equal to 'linear' or 'corotational' for linear and corotational geometry, resp.
Cross-Reference Information
This function calls:
- DefGeom_Quad determines local coordinates and corotational triad of quadrilateral element
- Large3du2ul_Quad determine the local displacements of a triangular element
- Rot2q convert normalized rotation vector to quaternion representation
- q2Rmat determine rotation matrix from normalized quaternions
- spin determine the spin tensor of a vector
- spinblk determine the spin tensors for a group of vectors
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- LE4nodeMindlinPlate linear elastic isoparametric 4-node quadrilateral Mindlin plate element
- LE4nodeMindlinPlatewITC linear elastic isoparametric 4-node quadrilateral Mindlin plate element with ITC
- LE4nodeMindlinShellwITC linear elastic isoparametric 4-node quadrilateral Mindlin shell element with ITC
- LE4to9nodeMindlinPlate linear elastic isoparametric 4-9 node quadrilateral Mindlin plate element
- LE4to9nodeMindlinShell linear elastic isoparametric 4-9 node quadrilateral Mindlin shell element