Function on a triangle translating the basis

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: ted with the vertices, the next three are quadratic corrections at the midsides, the next three are cubic corrections at the midsides, and the last is a cubic \bubble function" associated with the centroid (Figure 5.5.2). An array implementation, as described by (5.5.6) and Examples 5.5. 1 and 5.5.2, may be the simplest data structure however, implementations with structures linked to geometric entities (Section 5.3) are also possible. Substituting the polynomial representation (5.5.6) into the transformed strain energy expression (5.5.4b) and external load (5.5.4a) yields Ae(V U ) = dT (Ke + Me)ce e (5.5.7a) 28 Mesh Generation and Assembly η 1 03 1 0 1 6, 9 0 1 0 1 05, 8 1 0 1 010 1 0 1 0 1 0 1 0 1 0 1 4, 7 1 0 1 0 ξ 2 Figure 5.5.2: Shape function placement and numbering for a hierarchical cubic approximation on a canonical right 45 triangle. (V f )e = dT fe e where K= ZZ e (5.5.7b) g1eN NT + g2e(N NT + N NT ) + g3eN NT ] det(Je)d d (5.5.8a) 0 M= ZZ e qNNT det(Je)d d (5.5.8b) Nf det(J )d d : (5.5.8c) 0 f= ZZ e e 0 Here, Ke and Me are the element sti ness and mass matrices and fe is the element load vector. Numerical integration will generally be necessary to evaluate these arrays when the coordinate transformation is not linear and we will study procedures to do this in Chapter 6. Element mass and sti ness matrices and load vectors are generated for all elements in the mesh and assembled into their proper locations in the global sti ness and mass matrix and load vector. The positions of the elemental matrices and vectors in their global counterparts are determined by their indexing. In order to illustrate this point, consider a linear shape function on an element with Vertices 4, 7, and 8 as shown in Figure 5.5.3. These vertex indices are mapped onto local indices, e.g., 1, 2, 3, of the canonical element and the correspondence is recorded as shown in Figure 5.5.3. After generating the element matrices and vectors, the global indexing determines where to add 5.5. Element Matrices and Their Assembly 29 these entries into the global sti nes and mass matrix and load v...
View Full Document

This document was uploaded on 03/16/2014 for the course CSCI 6860 at Rensselaer Polytechnic Institute.

Ask a homework question - tutors are online