Analysis of Simple Structures

An introduction to planar trusses, frames, and machines, including vital theoretical assumptions and analytical methods for architectural applications.

Overview

This module covers planar trusses, frames, and machines, detailing the theoretical assumptions required for manual analysis and the Methods of Joints and Sections. Trusses are a fundamental architectural element, allowing engineers to span massive distances—like stadium roofs and aircraft hangars—with minimal material weight.

Introduction to Planar Trusses

An overview of the geometry and structural behavior of trusses.

Truss

A truss is a rigid structural framework composed entirely of straight, slender members (like steel angles, tubes, or timber chords) joined together at their endpoints to form a continuous series of interlocking triangles.

The Power of Triangulation

By arranging members exclusively in triangles, the truss acts as a very deep, extremely lightweight beam. The triangle is the only 2D polygon that is inherently geometrically stable; it cannot change shape without physically altering the length of one of its sides. A rectangle, by contrast, will easily collapse into a parallelogram under lateral load unless cross-braced (which simply turns it into two triangles).

Assumptions in Truss Analysis

The theoretical mathematical simplifications that make manual truss analysis possible.

Simplifying the Reality

To mathematically calculate the internal forces inside a truss by hand, structural engineers must make three vital assumptions that simplify the complex physical reality into a solvable mathematical model:
  • 1. Members are joined by smooth, frictionless pins: We mathematically assume the connections cannot resist bending moments (even if they are heavily welded steel gusset plates in reality). They are analyzed as if they act like freely rotating door hinges.
  • 2. Loads are applied ONLY at the joints: We never apply a load directly to the middle of a truss member. For example, in a real building, the heavy roof decking rests on horizontal purlins, and those purlins must rest only directly above the exact pin joints of the supporting truss.
  • 3. Member weight is negligible: The dead weight of the individual slender members is assumed to be negligible compared to the massive applied external loads (like snow or wind). If the self-weight is too large to ignore, half the member's weight is mathematically applied as a point load to the joints at each end of the member.

Important

The Resulting Two-Force Members: Because of these three strict assumptions, every single member in a theoretical truss is mathematically a two-force member. This means the member is either in pure Tension (being pulled apart axially) or pure Compression (being crushed together axially). There is absolutely zero internal bending moment or shear force inside any member.

Zero-Force Members

Identifying members that carry no mathematical load to drastically simplify truss analysis.

Why have members with zero force?

Truss analysis often reveals that certain members carry exactly zero force under specific loading conditions. These are called Zero-Force Members. Why are they physically built into the real truss if they carry no load? They are required for overall geometric stability, to prevent long slender compression members from buckling out of plane, or to handle unexpected dynamic loads (like shifting wind directions or earthquakes).
Identifying Zero-Force Members by Inspection:
  • Case 1 (Two Non-Collinear Members): If a joint connects exactly two non-collinear members, and there is NO external load or support reaction applied at that specific joint, BOTH members are zero-force members.
  • Case 2 (Three Members, Two Collinear): If a joint connects exactly three members, and two of them are collinear (form a perfectly straight line), and there is NO external load or support reaction applied at that joint, the third (non-collinear) member is a zero-force member.

Rules for Zero-Force Members

Identifying Zero-Force Members

Architectural trusses often contain structural members that mathematically carry zero internal force under a specific loading condition. Identifying them immediately simplifies the structural analysis equations. They provide critical stability to long, slender compression members to prevent sudden geometric buckling.

Procedure

  1. Two-Member Joints: If a joint physically connects exactly two distinct non-collinear structural members, and there is mathematically zero external load and zero external reaction force applied at that specific joint, then both structural members must mathematically carry zero internal force (F=0F = 0).
  2. Three-Member Joints: If a joint physically connects exactly three structural members, where two of the members are mathematically collinear (sharing the exact same straight line), and there is zero external load applied at the joint, then the third non-collinear member must mathematically carry zero internal force (F=0F = 0).

The Method of Joints

A systematic procedure for determining the internal axial force in every single member of a truss.

Analyzing Node by Node

The Method of Joints is the required analytical method when an engineer needs to find the internal force in every single member of the entire truss framework.
The Concept: Since the entire global truss is in static equilibrium, every individual internal joint (node) must also be in perfect equilibrium. By isolating a single joint, we can treat it as a 2D Concurrent Force System. Because all forces pass through the pin, there are no moments to calculate (ΣM=0\Sigma M = 0 is naturally satisfied).

Procedure

Method of Joints Steps:
  • Step 1: Calculate the external support reactions for the entire truss using global equilibrium (ΣFx=0,ΣFy=0,ΣM=0\Sigma F_x = 0, \Sigma F_y = 0, \Sigma M = 0).
  • Step 2: Pick a starting joint that has at most two unknown member forces (usually located at the supports). You cannot solve a joint with three unknowns because you only have two equations available.
  • Step 3: Draw a Free Body Diagram (FBD) of that isolated joint. Crucial Tip: Always draw unknown member force arrows pointing away from the joint (assuming they are in Tension).
  • Step 4: Apply ΣFx=0\Sigma F_x = 0 and ΣFy=0\Sigma F_y = 0 to solve for the two unknown forces.
  • Step 5: Check the sign of your answer. If the math yields a positive (++) number, your tension assumption was correct. If it yields a negative (-) number, the member is actually in Compression.
  • Step 6: Move to the next adjacent joint that now has only two unknowns remaining, and repeat until all members are solved.

The Method of Sections

An efficient mathematical technique for isolating and calculating internal forces in a few specific truss members.

Slicing the Truss

The Method of Sections is used when you only need to find the forces in a few specific members (often located near the middle of a long truss). It is drastically faster than the Method of Joints because it bypasses the need to calculate every single joint sequentially from the support.
The Concept: Instead of isolating a single concurrent joint, we draw an imaginary line slicing completely through the entire truss, cutting the specific members we want to analyze. This divides the truss into two separate rigid bodies. We discard one half and apply full rigid body equilibrium to the remaining half.

Procedure

Method of Sections Steps:
  • Step 1: Calculate the external support reactions for the entire global truss.
  • Step 2: Draw an imaginary line cutting completely through the truss. The line must cut through the specific members you want to find. Ensure you cut no more than three members whose internal forces are unknown (because you only have three equilibrium equations).
  • Step 3: Discard one half of the cut truss. Draw an FBD of the remaining half.
  • Step 4: At the cut ends, draw arrows representing the internal forces of the cut members, assuming they act in Tension (pulling away from the cut surface).
  • Step 5: Apply the three rigid body equilibrium equations (ΣFx=0\Sigma F_x = 0, ΣFy=0\Sigma F_y = 0, ΣM=0\Sigma M = 0) to the remaining half to solve for the three unknown cut members.

Important

Pro Tip for Sections: Taking a moment equation (ΣM=0\Sigma M = 0) about a point in space where two of the unknown cut members intersect is a highly powerful trick. Because their lines of action pass through the moment center, their moment arms are zero. This instantly eliminates them from the equation, allowing you to solve directly for the third unknown member in a single line of math!

Frames and Machines

Analyzing structural systems that resist bending moments and handle multi-force members.

Beyond Trusses

While trusses are incredibly efficient, many common architectural structures (like modern high-rise portal frames, A-frame cabins, and mechanical construction equipment) do not meet the strict assumptions of a pure truss. These are classified as Frames or Machines.
  • Frames vs. Trusses: Unlike trusses (which only have two-force members), Frames must contain at least one multi-force member. A multi-force member has loads applied along its length (not just at the joints), meaning it actively resists significant internal bending moments and shear forces.
  • Machines: A Machine is essentially a moving frame. It is designed specifically to transmit or mechanically alter forces. They generally have moving parts and frequently use pinned connections to transfer massive loads, much like construction cranes or heavy-duty excavators used on architectural sites.
Method of Members: To analyze a frame or machine, you cannot simply isolate a point using the Method of Joints. Instead, you must carefully dismantle the entire physical structure into individual Free Body Diagrams (FBDs) for each separate member. Then, you apply the three rigid body equilibrium equations (ΣFx=0\Sigma F_x=0, ΣFy=0\Sigma F_y=0, ΣM=0\Sigma M=0) to each multi-force member independently.

Caution

Newton's Third Law is Critical: When dismantling a frame to draw individual FBDs, Action and Reaction must be strictly observed. If Member A pushes down and to the right on Member B at a connecting pin, Member B must push up and to the left on Member A with the exact same force magnitude at that same pin. Mixing up these signs is the most common error in frame analysis.

Ideal vs. Real Joints

The divergence between theoretical truss assumptions and actual construction.

Gusset Plates and Secondary Stresses

Standard truss analysis fundamentally assumes that all joints are perfectly frictionless pins, meaning members only experience pure axial tension or compression.
In real architectural construction, steel trusses are bolted or welded together using large, thick metal plates called gusset plates. These rigid connections prevent the members from rotating freely. As the truss deflects slightly under a heavy roof load, the stiff gusset plates force the members to bend, inducing "secondary bending moments" alongside the primary axial forces. While often small enough to ignore in preliminary design, these secondary stresses must be verified in final engineering calculations.

Advanced Concepts

Supplemental theoretical knowledge required for comprehensive architectural mechanics.

Space Trusses

While 2D planar trusses are common, modern stadiums and airports utilize 3D Space Trusses consisting of tetrahedral units. Analysis requires extending the Method of Joints into three dimensions (XX, YY, and ZZ) simultaneously.

Assumptions of an Ideal Truss

The strict mathematical rules that define a perfectly theoretical truss framework.

The Three Ideal Assumptions

To simplify hand calculations, structural engineers treat real-world trusses as "ideal" models by enforcing three strict mathematical assumptions:
  1. All members are perfectly straight slender bodies connected at their absolute endpoints. If a member is naturally curved, it will inherently experience internal bending, violating the definition of a truss.
  2. All joints are completely frictionless pins. Real trusses use heavy welded gusset plates that resist rotation. By assuming frictionless pins, we guarantee the joints cannot transmit moments, forcing the members to carry only axial loads.
  3. All external loads and support reactions are applied exactly at the joints. If a heavy ceiling fan is hung from the exact middle of a bottom truss chord, that specific member becomes a multi-force member experiencing heavy bending, invalidating the simple truss analysis for that piece.

Method of Joints vs. Sections

Choosing the correct analytical approach based on the specific architectural problem.

Which Method to Use?

  • Use the Method of Joints when you need a comprehensive analysis of the entire structure. It is systematic and exhaustive, making it the mathematical basis for all modern structural computer software. However, calculating a massive 100-member stadium truss entirely by hand using this method is unfeasible.
  • Use the Method of Sections when you only need to verify the maximum stress in a few critical members (usually near the mid-span of the truss where bending forces are highest). It is mathematically elegant and fast, allowing engineers to spot-check computer results quickly.
Key Takeaways
  • Trusses are rigid frameworks made exclusively of straight slender members assembled in triangles, carrying loads purely in axial tension or compression.
  • Truss analysis requires three assumptions: frictionless pins, loads applied only at joints, and negligible member weight.
  • Zero-force members carry no axial load under a specific loading condition but provide geometric stability against buckling.
  • The Method of Joints is used to find forces in all members by isolating concurrent joint nodes (ΣFx=0,ΣFy=0\Sigma F_x = 0, \Sigma F_y = 0).
  • The Method of Sections is used to find forces in specific members by cutting the truss and applying full rigid body equilibrium (ΣM=0\Sigma M = 0).
  • Frames and Machines contain multi-force members that resist bending, requiring the entire structure to be dismantled into individual FBDs for analysis.