Examples & Applications

Step-by-step applications of the Direct Stiffness Method to different structural systems, followed by conceptual case studies.

Numerical Examples

Example 1: 2D Truss Analysis

Consider a simple 2-bar planar truss. Node 1 is a pin support at (0,0)(0, 0). Node 2 is a pin support at (L,0)(L, 0). Node 3 is a free joint at (L/2,H)(L/2, H), subjected to a downward vertical load PP. Both members have cross-sectional area AA and modulus of elasticity EE. We want to set up the global stiffness matrix and solve for displacements.

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Example 2: 2-Span Continuous Beam

Analyze a 2-span continuous beam. Span 1 (Node 1 to Node 2) has length LL and flexural rigidity EIEI. Span 2 (Node 2 to Node 3) has length LL and flexural rigidity EIEI. Nodes 1, 2, and 3 are roller/pin supports preventing vertical translation. A uniformly distributed load ww is applied over Span 1.

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Example 3: 2D Portal Frame Assembly

Consider a simple 2D portal frame consisting of two vertical columns (height HH) and a horizontal beam (length LL). The bases of the columns (Nodes 1 and 4) are fixed. The beam connects Nodes 2 and 3. All members have properties AA, EE, II. Formulate the global stiffness matrix conceptually.

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Case Studies: Matrix Analysis in Practice

Case Study 1: Commercial Structural Software (SAP2000, ETABS)

Modern commercial structural analysis software operates entirely on the principles of the Direct Stiffness Method. When an engineer draws a line representing a beam and assigns it a steel section, the software internally calculates the A,I,EA, I, E properties, formulates the local stiffness matrix, determines the transformation matrix based on the drawn orientation, and assembles the global [K][K] matrix.
The efficiency of the matrix method allows these programs to solve models with hundreds of thousands of degrees of freedom in seconds. The software also handles complex boundary conditions (like spring supports, which simply add values to the diagonal terms of the [K][K] matrix) and rigid diaphragms (which kinematically constrain the DOFs of floor nodes together, reducing the total number of equations to solve).

Case Study 2: Dynamic and Non-linear Extensions

The fundamental stiffness equation {P}=[K]{D}\{P\} = [K]\{D\} is the starting point for more advanced analyses.
In structural dynamics (e.g., earthquake engineering), a mass matrix [M][M] and damping matrix [C][C] are assembled using similar systematic procedures. The static equation is expanded into the equation of motion: [M]{D¨}+[C]{D˙}+[K]{D}={P(t)}[M]\{\ddot{D}\} + [C]\{\dot{D}\} + [K]\{D\} = \{P(t)\}.
In non-linear analysis (e.g., yielding steel, large deflections), the stiffness matrix [K][K] is no longer constant. It must be updated iteratively as the structure deforms or members yield, demonstrating the flexibility and power of matrix formulations to adapt to complex structural behaviors.