Faculty of Engineering
Mechanical Engineering Department
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan                   1
        Introduction
      This chapter introduces some of the basic concepts on which the direct
       stiffness method is derived.
      The linear spring is introduced first because it provides a simple instructive
       tool to illustrate the basic concepts.
      We begin with the derivation of the stiffness matrix for a linear-elastic spring
       element.
      We next illustrate how to assemble the total stiffness matrix for a structure.
      After establishing the total structure stiffness matrix, we illustrate how to
       impose boundary conditions.
      A complete solution including the nodal displacements and reactions is thus
       obtained.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan               2
        Direct Stiffness Method
        To Derive Spring Element Equations
          Step 1: Select the Element Type
          Consider the linear spring element (which can be an element in a system of
          springs) subjected to resulting nodal tensile forces T
          The local 𝑥 axis is directed from node 1 to node 2. The original distance
          between nodes before deformation is denoted by L. The material property
          (spring constant) of the element is k.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan            3
        Direct Stiffness Method
        To Derive Spring Element Equations
          Step 2: Select a Displacement Function
           We must choose in advance the mathematical function to represent the
           deformed shape of the spring element under loading. The most common
           functions used are polynomials.          𝒖=𝒂 +𝒂 𝒙                  𝟏   𝟐
           In general, the total number of coefficients a is equal to the total number of
           degrees of freedom associated with the element. Here the total number of
           degrees of freedom is two. In matrix form,                       𝒂𝟏
                                                                       𝒖= 𝟏 𝒙 𝒂
                                                                               𝟐
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan                 4
        Direct Stiffness Method
        To Derive Spring Element Equations
          Step 2: Select a Displacement Function
         We now want to express 𝒖 as a function of the nodal displacements 𝒅𝟏𝒙
         and 𝒅𝟐𝒙 . We achieve this by evaluating 𝑢 at each node and solving for 𝑎1
         and 𝑎2 as follows:
                                                                                𝑥     𝑥
                                                                         𝑢 = 1−   𝑑 +   𝑑
                                                                                𝐿 1𝑥  𝐿 2𝑥
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan                  5
        Direct Stiffness Method
        To Derive Spring Element Equations
         Step 2: Select a Displacement Function
         In matrix form,
            Here N1 and N2 are called the shape functions or often called interpolation
            functions. In this case, N1 and N2 are linear functions that have the
            properties that N1 = 1 at node 1 and N1 = 0 at node 2, whereas N2 = 1 at
            node 2 and N2 = 0 at node 1.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan               6
        Direct Stiffness Method
        To Derive Spring Element Equations
      Step 3: Define the Strain/ Displacement and Stress/Strain Relationships
      The deformation of the spring is then represented by:
      The stress/strain relationship can be expressed in terms of the force/deformation
      relationship instead as:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan               7
        Direct Stiffness Method
        To Derive Spring Element Equations
        Step 4: Derive the Element Stiffness Matrix and Equations
        We now derive the spring element stiffness matrix. By the sign convention for
        nodal forces and equilibrium, we have:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan             8
        Direct Stiffness Method
        To Derive Spring Element Equations
        Step 4: Derive the Element Stiffness Matrix and Equations
        In matrix form,
        We obtain,
        Here k is called the local stiffness matrix for the element.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan   9
        Direct Stiffness Method
        To Derive Spring Element Equations
      Step 5: Assemble the Element Equations to Obtain the Global
      Equations and Introduce Boundary Conditions
      The global stiffness matrix and global force matrix are assembled using nodal
      force equilibrium equations. This step applies for structures composed of more
      than one element such that
        where k and f are now element stiffness and force matrices expressed in a
        global reference frame.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan            10
        Direct Stiffness Method
        To Derive Spring Element Equations
      Step 6: Solve for the Nodal Displacements
       The displacements are then determined by imposing boundary conditions, such
       as support conditions, and solving a system of equations, F = Kd,
       simultaneously.
      Step 7: Solve for the Element Forces
       Finally, the element forces are determined by back-substitution, applied to each
       element.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan               11
        Direct Stiffness Method
        Example of a Spring Assemblage
       Structures such as trusses, building frames, and bridges include basic structural
       components connected to form the overall structures.
       To analyze these structures, we must determine the total structure stiffness
       matrix for the interconnected system of elements.
       Consider the system of two springs below:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan                12
        Direct Stiffness Method
        Example of a Spring Assemblage
        Here we fix node 1 and apply axial forces for F3x at node 3 and F2x at node 2.
        The stiffnesses of spring elements 1 and 2 are k1 and k2, respectively.
        The nodes of the assemblage have been numbered 1, 3, and 2 for further
        generalization because sequential numbering between elements generally does
        not occur in large problem
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan              13
        Direct Stiffness Method
        Example of a Spring Assemblage
         For element 1, using the Eq. developed before, we have:
         And for element 2, we have:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan   14
        Direct Stiffness Method
        Example of a Spring Assemblage
         Furthermore, elements 1 and 2 must remain connected at common node 3
          throughout the displacement. This is called the continuity or compatibility
          requirement. The compatibility requirement yields:
         Based on the fact that external forces must equal internal forces at each
          node, we can write nodal equilibrium equations at nodes 3, 2, and 1 as:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan             15
        Direct Stiffness Method
        Example of a Spring Assemblage
         Now we can write the displacements in matrix form as:
                                        is called the global nodal displacement matrix.
         And we can write the forces in matrix form as:
                                        is called the global nodal force matrix.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan               16
        Direct Stiffness Method
        Example of a Spring Assemblage
         Aassembling the Total Stiffness Matrix by Superposition
          The element stiffness matrices are given as:
         K is then constructed simply by directly adding terms as:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan   17
        Direct Stiffness Method
        Example of a Spring Assemblage
         Boundary Conditions:
         Here we have d1x = 0 because node 1 is fixed. F1x is the unknown reaction
          and F2x and F3x are known applied loads. Therefore, we can write:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan           18
        Direct Stiffness Method
        Example of a Spring Assemblage                                        Solving
           For all homogeneous boundary conditions, we can delete the rows and
            columns corresponding to the zero-displacement from the original set of
            equations and then solve for the unknown displacements. This
            procedure is useful for hand calculations. (computer can be used for
            solving the system of simultaneous equations.)
           F1x is not necessarily zero and can be determined once d2x and d3x are
            solved for.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan             19
        Example 2.1:
        For the spring assemblage with arbitrarily numbered nodes shown in Figure
        below, using direct stiffness method obtain (a) the global stiffness matrix, (b)
        the displacements of nodes 3 and 4, (c) the reaction forces at nodes 1 and 2,
        and (d) the forces in each spring. A force of 5000 lb is applied at node 4 in the
        x direction. The spring constants are given in the figure. Nodes 1 and 2 are
        fixed.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan                 20
        Example 2.1:
        (a). We begin by expressing each element stiffness matrix as follows:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan     21
        Example 2.1:
        Using the concept of superposition (the direct stiffness method), we obtain the
        global stiffness matrix as:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan               22
        Example 2.1:
        (b). The global stiffness matrix relates global forces to global displacements as
        follows:
        Applying the boundary conditions d1x=0 and d2x=0, substituting applied nodal
        forces, and deleting the first two rows of {F} and {d} and the first two rows and
        columns of [K] corresponding to the zero-displacement boundary conditions,
        we obtain:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan                 23
        Example 2.1:
        (c). To obtain the global nodal forces which include the reactions at nodes 1
        and 2, we back-substitute and the boundary conditions d1x=0 and d2x=0. This
        substitution yields:
        Multiplying matrices and simplifying, we obtain the forces at each node,
        From these results, we observe that the sum of the reactions F1x and F2x is
        equal in magnitude but opposite in direction to the applied force F4x. This
        result verifies equilibrium of the whole spring assemblage.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan             24
        Example 2.1:
        Next, we use local element Eqs. to obtain the forces in each element.
        By simplifying, we obtain,
        A free-body diagram of spring element 1 is shown in Figure (a) below. The
        spring is subjected to tensile forces. Also, ^f1x is equal to the reaction force
        F1x. A free-body diagram of node 1, Figure (b) shows this result.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan                25
        Example 2.1:
        By simplifying, we obtain,
        A free-body diagram of spring element 2 is shown in Figure below. The spring
        is subjected to tensile forces.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan            26
        Example 2.1:
        By simplifying, we obtain,
        A free-body diagram of spring element 3 is shown in Figure (a) below. The
        spring is subjected to compressive forces. Also, ^f2x is equal to the reaction
        force F2x. A free-body diagram of node 2, Figure (b) shows this result.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan              27
        Example 2.2:
        For the spring assemblage shown in Figure below, using direct stiffness
        method obtain (a) the global stiffness matrix, (b) the displacements of nodes
        2–4, (c) the global nodal forces, and (d) the local element forces. Node 1 is
        fixed while node 5 is given a fixed, known displacement d = 20 mm. The
        spring constants are all equal to k = 200 kN/m
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan             28
        Example 2.2:
        (a). We express each element stiffness matrix as follows:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan   29
        Example 2.2:
        Again, using superposition, we obtain the global stiffness matrix as:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan     30
        Example 2.2:
        (b).   The global stiffness matrix relates the global forces to the global
        displacements as follows:
        Applying the boundary conditions d1x=0 and d5x=20 mm (= 0.02 m), deleting
        the first and fifth equations corresponding to these boundary conditions, and
        substituting known global forces F2x=0, F3x=0, and F4x=0, we obtain:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan             31
        Example 2.2:
        We now rewrite Eqs. transposing the product of the appropriate stiffness
        coefficient (-200) multiplied by the known displacement (0.02 m) to the left
        side.
        Solving the above Eqs., we obtain:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan            32
        Example 2.2:
        (c). The global nodal forces are obtained by back-substituting the boundary
        condition displacements. This substitution yields,
        The results yield the reaction F1x opposite that of the nodal force F5x required
        to displace node 5 by d = 20 mm. This result verifies equilibrium of the whole
        spring assemblage.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan                33
        Example 2.2:
        (d). Next, we use local element Eqs. to obtain the forces in each element.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan          34
        Example 2.2:
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan   35
        Example 2.3:
        Using the direct stiffness method, formulate the global stiffness matrix and
        equations for solution of the unknown global displacements and forces. The
        spring constants for the elements are k1; k2, and k3; P is an applied force at
        node 2.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan              36
        Example 2.3:
        Using the direct stiffness method, we formulate the global stiffness matrix.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan            37
        PROBLEMS
        For the spring assemblages shown in Figures P2–12 to P2–13, determine the
        nodal displacements, the forces in each element, and the reactions. Use the
        direct stiffness method for all problems.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan           38
        PROBLEMS
        For the spring assemblages shown in Figures P2–15 to P2–16, determine the
        nodal displacements, the forces in each element, and the reactions. Use the
        direct stiffness method for all problems.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan           39
        Assignment #2a
        For the spring assemblages shown in Figures P2–8 to P2–11, determine the
        nodal displacements, the forces in each element, and the reactions. Use the
        direct stiffness method for all problems.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan           40
        Variational Method
        (Potential Energy Approach)
        One of the alternative methods often used to derive the element equations
        and the stiffness matrix for an element is based on the principle of minimum
        potential energy. The principle of minimum potential energy is applicable
        only for elastic materials .
        Total potential energy (p) is defined as the sum of the internal strain energy
        (U) and the potential energy of the external forces (); that is,
                                                𝝅𝒑 = 𝑼 + 𝜴
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan               41
        Potential Energy Approach
        To Derive Spring Element Equations
        Internal Strain Energy (U):
        The differential internal work (or strain energy) dU in the spring for a small
        change in length of the spring is the internal force multiplied by the change
        in displacement through which the force moves, given by: 𝒅𝑼 = 𝑭𝒅𝒙
        Now we express F as, 𝑭 = 𝒌𝒙
        The differential strain energy becomes, 𝒅𝑼 = 𝒌𝒙𝒅𝒙
                                                                              𝒙
        The total strain energy is then given by, 𝒅𝑼 =                            𝒌𝒙𝒅𝒙
                                                                              𝟎
        Upon integration, we obtain,                𝟏 𝟐
                                                 𝑼 = 𝒌𝒙
                                                    𝟐
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan              42
        Potential Energy Approach
        To Derive Spring Element Equations
        The potential energy of the external forces ():
        The potential energy of the external force is lost when the work is done by
        the external force and it is given by,
                                                          𝜴 = −𝑭𝒙
                                                                                  𝟏 𝟐
        Now evaluate The Total Potential Energy (p) as:                      𝝅𝒑 = 𝒌𝒙 − 𝑭𝒙
                                                                                  𝟐
        Minimization of (p) through standard mathematics by taking the variation
        of (p) with respect to x as,      𝜕𝜋𝑝
                                                                   =0
ME 646, Dr. Hafeth Bu Jldain,
                                                            𝜕𝑥
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan              43
        Potential Energy Approach
        To Derive Spring Element Equations
        We now derive the spring element equations and stiffness matrix using the
        principle of minimum potential energy. Consider the linear spring subjected
        to nodal forces shown in the Figure.
                         1                           2
                     𝜋𝑝 = 𝑘 𝑑2𝑥 − 𝑑1𝑥                    − 𝑓1𝑥 𝑑1𝑥 − 𝑓2𝑥 𝑑2𝑥
                         2
                         1   2                2
                     𝜋𝑝 = 𝑘 𝑑2𝑥 − 2𝑑2𝑥 𝑑1𝑥 + 𝑑1𝑥 − 𝑓1𝑥 𝑑1𝑥 − 𝑓2𝑥 𝑑2𝑥
                         2
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan           44
        Potential Energy Approach
        To Derive Spring Element Equations
        The minimization of (p) with respect to each nodal displacement requires
        taking partial derivatives of (p) with respect to each nodal displacement such
        that:           𝜕𝜋         1
                                  𝑝
                                       = 𝑘 −2𝑑2𝑥 + 2𝑑1𝑥 − 𝑓1𝑥 = 0
                                𝜕𝑑1𝑥    2
                                𝜕𝜋𝑝     1
                                       = 𝑘 2𝑑2𝑥 − 2𝑑1𝑥 − 𝑓2𝑥 = 0
                                𝜕𝑑2𝑥    2
        Simplifying,            𝑘 −𝑑2𝑥 + 𝑑1𝑥 = 𝑓1𝑥
                                 𝑘 𝑑2𝑥 − 𝑑1𝑥 = 𝑓2𝑥
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan               45
        Potential Energy Approach
        To Derive Spring Element Equations
        Rewriting them as,                 𝑘 𝑑1𝑥 − 𝑑2𝑥 = 𝑓1𝑥
                                         𝑘 −𝑑1𝑥 + 𝑑2𝑥 = 𝑓2𝑥
        In matrix form,
                                           𝑘         −𝑘       𝑑1𝑥   𝑓1𝑥
                                                                  =
                                           −𝑘        𝑘        𝑑2𝑥   𝑓2𝑥
        Then, the stiffness matrix for the spring element is,
                                                         𝑘        −𝑘
                                             [𝑘 ] =
                                                         −𝑘       𝑘
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan   46
        Example 2.5:
        Obtain the total potential energy of the spring assemblage shown in the Figure
        below and find its minimum value. The procedure of assembling element
        equations shall be obtained from the minimization of the total potential
        energy.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan              47
        Example 2.5:
        The total potential energy is given by:
                        3
                                 (𝑒)    1                       2             1       1
                                𝜋𝑝     = 𝑘1 𝑑3𝑥 − 𝑑1𝑥               − 𝑓1𝑥 𝑑1𝑥 − 𝑓3𝑥 𝑑3𝑥
                                        2
                     𝑒=1
                                 1                       2          2             2
                                + 𝑘2 𝑑4𝑥 − 𝑑3𝑥               − 𝑓3𝑥 𝑑3𝑥 − 𝑓4𝑥 𝑑4𝑥
                                 2
                                 1                       2          3             3
                                + 𝑘3 𝑑2𝑥 − 𝑑4𝑥               − 𝑓4𝑥 𝑑4𝑥 − 𝑓2𝑥 𝑑2𝑥
                                 2
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan               48
        Example 2.5:
        Upon minimizing (p) with respect to each nodal displacement, we obtain:
          𝜕𝜋𝑝                          (1)
               = −𝑘1 𝑑3𝑥 + 𝑘1 𝑑1𝑥 − 𝑓1𝑥 = 0
          𝜕𝑑1𝑥
          𝜕𝜋𝑝                        (3)
               = 𝑘3 𝑑2𝑥 − 𝑘3 𝑑4𝑥 − 𝑓2𝑥 = 0
          𝜕𝑑2𝑥
          𝜕𝜋𝑝                                          1     (2)
               = 𝑘1 𝑑3𝑥 − 𝑘1 𝑑1𝑥 − 𝑘2 𝑑4𝑥 + 𝑘2 𝑑3𝑥 − 𝑓3𝑥 − 𝑓3𝑥 = 0
          𝜕𝑑3𝑥
           𝜕𝜋𝑝                                          2     (3)
               = 𝑘2 𝑑4𝑥 − 𝑘2 𝑑3𝑥 − 𝑘3 𝑑2𝑥 + 𝑘3 𝑑4𝑥 − 𝑓4𝑥 − 𝑓4𝑥 = 0
          𝜕𝑑4𝑥
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan        49
        Example 2.5:
        By rearranging the previous equations, we obtain:
                                                        (1)
                       +𝑘1 𝑑1𝑥 −𝑘1 𝑑3𝑥 = 𝑓1𝑥
                                                       (3)
                      +𝑘3 𝑑2𝑥 − 𝑘3 𝑑4𝑥 = 𝑓2𝑥
                                                                              1   (2)
                      −𝑘1 𝑑1𝑥 + 𝑘1 + 𝑘2 𝑑3𝑥 − 𝑘2 𝑑4𝑥 = 𝑓3𝑥 + 𝑓3𝑥
                                                                              2   (3)
                       −𝑘3 𝑑2𝑥 − 𝑘2 𝑑3𝑥 + 𝑘2 + 𝑘3 𝑑4𝑥 = 𝑓4𝑥 + 𝑓4𝑥
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan             50
        Example 2.5:
      In matrix form become:                                                   (1)
                                                                              𝑓1𝑥
     𝑘1             0             −𝑘1              0          𝑑1𝑥                    𝐹1𝑥
                                                                           (3)
      0            𝑘3              0         −𝑘3              𝑑2𝑥       𝑓 2𝑥         𝐹2𝑥
                                                                  =                =
     −𝑘1            0           𝑘1 + 𝑘2       −𝑘2             𝑑3𝑥     (1)
                                                                    𝑓3𝑥 + 𝑓3𝑥
                                                                               (2)   𝐹3𝑥
      0            −𝑘3           −𝑘2        𝑘2 + 𝑘3           𝑑4𝑥     (2)      (3)   𝐹4𝑥
                                                                    𝑓4𝑥 + 𝑓4𝑥
      By substituting numerical values we obtain,
      1000    0   −1000     0                                          𝑑1𝑥   𝐹1𝑥
        0   3000  0     −3000                                          𝑑2𝑥   𝐹2𝑥
                                                                           =
      −1000   0   3000 −2000                                           𝑑3𝑥   𝐹3𝑥
        0   −3000 −2000 5000                                           𝑑4𝑥   𝐹4𝑥
      When we apply the boundary conditions and substitute F3x = 0 and F4x = 5000 lb,
      the solution is identical to that of Example 2.1.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan                51
        PROBLEMS
        Using P.E. approach to solve next Problems.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan   52
        Assignment #2b
        Using P.E. approach to solve next Problems.
ME 646, Dr. Hafeth Bu Jldain,
A First Course in the Finite Element Method, Fourth Edition, Daryl L. Logan   53
Thank you
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