Page 49 - Fundamentals of The Finite Element Method for Heat and Fluid Flow
P. 49

41
                        THE FINITE ELEMENT METHOD
                        3. Form element equations (Formulation)
                           Next, we have to determine the matrix equations that express the properties of the
                        individual elements by forming an element Left Hand Side (LHS) matrix and load vector.
                        For example, a typical LHS matrix and a load vector can be written as
                                                          Ak     1 −1
                                                   [K] e =                                   (3.1)
                                                           l  −1   1

                                                           Q i
                                                    {f} e =                                  (3.2)
                                                           Q j
                        where the subscript e represents an element; Q is the total heat transferred; k is the thermal
                        conductivity; l is the length of a one-dimensional linear element and i and j represent the
                        nodes forming an element. The unknowns are the temperature values on the nodes.
                        4. Assemble the element equations to obtain a system of simultaneous equations
                           To find the properties of the overall system, we must assemble all the individual ele-
                        ment equations, that is, to combine the matrix equations of each element in an appropriate
                        way such that the resulting matrix represents the behaviour of the entire solution region
                        of the problem. The boundary conditions must be incorporated after the assemblage of the
                        individual element contributions (see Appendix C), that is,

                                                       [K]{T}={f}                            (3.3)

                        where [K] is the global LHS matrix, which is the assemblage of the individual element LHS
                        matrices, as given in Equation 3.1, {f} is the global load vector, which is the assemblage of
                        the individual element load vectors the Equation 3.2, and {T} is the global unknown vector.
                        5. Solve the system of equations
                           The resulting set of algebraic equations, Equation 3.3, may now be solved to obtain the
                        nodal values of the field variable, for example, temperature.
                        6. Calculate the secondary quantities
                           From the nodal values of the field variable, for example, temperatures, we can then
                        calculate the secondary quantities, for example, space heat fluxes.


                        3.2 Elements and Shape Functions

                        As shown in Figure 3.1, the finite element method involves the discretization of both the
                        domain and the governing equations. In this process, the variables are represented in a
                        piece-wise manner over the domain. By dividing the solution region into a number of
                        small regions, called elements, and approximating the solution over these regions by a
                        suitable known function, a relation between the differential equations and the elements is
                        established. The functions employed to represent the nature of the solution within each
                        element are called shape functions, or interpolating functions, or basis functions. They are
                        called interpolating functions as they are used to determine the value of the field variable
                        within an element by interpolating the nodal values. They are also known as basis functions
                        as they form the basis of the discretization method. Polynomial type functions have been
   44   45   46   47   48   49   50   51   52   53   54