Understanding and Analysing Trusses

Trusses are important structures in engineering that are used in all sorts of applications, from bridges and roofs to parts of the International Space Station. The reason they are so useful is that they allow us to create strong and rigid structures while using materials in a very efficient way.

This page will cover everything you need to know to understand and analyse trusses, but you can also watch the video below for the animated version!

What is a truss?

A truss in everyday language is a rigid structure that is made up of a collection of straight members. But in an engineering and strength of materials context it has a more specific meaning – in these contexts a truss is a structure made up of members that only carry axial loads.

The members of a structure can be considered to only carry axial loads if the following assumptions are applicable:

Assumption 1

The joints of the structure behave like pinned connections

Assumption 2

Loads are only applied at the joints of the structure

If these assumptions can be applied, the truss members are not acted on by any bending moments – they only carry axial loads. This means that each member of a truss must be either in tension or in compression.

Truss members can only carry axial loads so they are either in tension or in compression

The fact that truss members only carry axial loads makes the analysis of trusses much easier than the analysis of frames, for example, where the members can carry both bending moments and axial loads.

Truss on the left (pinned connections and loads acting at joints only) and frame on the right (rigid connections and loads acting in the middle of a member)

When can a structure be analysed as a truss?

Few real structures have actual pinned connections, so how do you decide if you can analyse a real structure as a truss?

The members of real structures like bridges are often rigidly connected using what is known as a gusset plate, a plate that is bolted or riveted to several structural members, as shown in the photograph below. If the centre-lines of all of the members at a joint intersect at the same point, then it is reasonable to assume that the joint behaves in a similar way to a pinned connection.

Gusset plates on a bridge

For analysis purposes it is often reasonable to assume that any loads carried by the structure can be modelled as acting at the joints, instead of being distributed over the length of the members. This is usually valid if the members are relatively short.

This means that structures like the bridge shown above can often be analysed as trusses.

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Truss stability

The base shape of a truss is three members connected to form a triangle. If a load is applied to the structure the angles of the triangle won’t be able to change if the length of each of the members stays the same. This means that the triangle is a very stable shape that won’t deform when loads are applied to it, and so it is a great base from which to build a larger structure.

Joining four members together does not form a stable structure. The angles between members can change without any change in the length of the members, so using a four-sided shape as the base for building a truss structure would be a terrible choice. An easy way to stabilize this configuration is to add a diagonal bracing member to split it into triangles.

Unstable configuration made stable by adding a diagonal member

The figure below shows some common truss designs, which as you can see are made up of triangular elements.

Common truss configurations

Analysing Trusses

When analysing a truss the main objective is to determine the force in each of its members for a certain set of applied loads. This allows us to check that the members can carry the loads without failing, or gives us the information we need to select the best cross-section for each of the members. There are two main methods we can use to do this – the Method of Joints, and the Method of Sections.

The Method of Joints

The method of joints involves applying the static equilibrium equations to the joints in the truss to determine the forces acting on each joint. From there the tensile or compressive axial force carried by each member of the truss can easily be determined.

Here’s how it works:

Step 1

Draw a free body diagram of the truss and solve reaction forces

The first step is to draw a free body diagram showing all of the external loads acting on the truss.

The reaction forces at the truss supports can then be calculated using the three static equilibrium equations.

$$\sum F_\leftrightarrow = 0$$ $$\sum F_\updownarrow = 0$$ $$\sum M = 0$$

Step 2

Draw a free body diagram of each joint and solve internal forces

The next step is to draw a free body diagram for every single joint, and work through them one by one to solve the unknown forces acting at the joint.

The unknown forces can be determined by once again applying the equilibrium equations. All of the joints are pinned connections so there are no moments – you only need to consider equilibrium of the horizontal and vertical forces. $$\sum F_\leftrightarrow = 0$$ $$\sum F_\updownarrow = 0$$

This calculation gives the forces imparted on each of the joints by the members of the truss. The force each member imparts on a joint is equal and opposite to the axial force within the member. If the force acting on a joint because of a specific member is acting away from the joint, it means that the member is in tension, and if the force is acting towards the joint it means that the member is in compression.

Remember that each member is carrying a uniform axial load. This means that if you know the force acting on the joint at one end of the member, the force acting on the joint at the other end of the member will be the same.

The method of joints is useful when you need to calculate the forces in all of the members in the truss, but sometimes you only need to determine the force in one or two members. In this case an alternative method, called the Method of Sections is quicker.

The Method of Sections

When using the Method of Sections, an imaginary cut is made through the truss. Beause the internal forces within the truss members develop in such a way that they balance the external forces (i.e. the reaction forces and the applied loads), the static equilibrium equations can be applied to determine the forces in the members that have been cut through.

Here’s a more detailed summary of the process:

Step 1

Draw a free body diagram of the truss and solve reaction forces

The first step is to draw a free body diagram showing all of the external loads acting on the truss. The three static equilibrium equations can be applied to calculate the reaction forces.

$$\sum F_\leftrightarrow = 0$$ $$\sum F_\updownarrow = 0$$ $$\sum M = 0$$

This is the exact same first step as for the Method of Joints.

Step 2

Cut the truss through the members of interest and draw the internal forces

The next step involves making an imaginary cut through the members of interest in the truss, and drawing the internal forces in the cut members.

Step 3

Apply the equilibrium equations to solve the internal forces

The internal forces and external forces will always be in equilibrium, no matter where you have decided to cut the truss. This means that the static equilibrium equations can be applied to solve the internal forces in the cut members.

$$\sum F_\leftrightarrow = 0$$ $$\sum F_\updownarrow = 0$$ $$\sum M = 0$$

The result of the calculation is the axial force in the members that have been cut through.

Related Topics

Shear Force and Bending Moment Diagrams

These diagrams are used to determine the distribution of shear force and bending moments along a beam, accounting for supports and loads.

Area Moment of Inertia

The area moment of inertia describes how the material of a cross-section is distributed relative to a specific bending axis.

Understanding and Analysing Trusses Read More »

Understanding the Area Moment of Inertia

The area moment of inertia, also called the second moment of area, is a parameter that defines how much resistance a shape (like the cross-section of a beam), has to bending because of its geometry.

Consider a thin plank that supports a 100 kg load. The plank will be much less stiff when the load is placed on the longer edge of the cross-section. This is because resistance to bending depends on how the material of the cross-section is distributed relative to the bending axis. The plank on the left has more material located further from the bending axis, which makes it much stiffer.

The same plank is much less stiff when the load is applied to the long edge of the cross-section. As we will soon see, this is related to the area moment of inertia.

This resistance to bending can be quantified by calculating the area moment of inertia of the cross-section. It is denoted using the letter $I$, has units of length to the fourth power, which is typically $mm^4$ or $in^4$. It reflects how the area of the cross section is distributed relative to a particular axis. It’s not a unique property of a cross section – it varies depending on the bending axis that is being considered.

Let’s compare $I$ values calculated for a few different cross-sections, for the bending axis shown below:

Area moment of inertia values (in mm4) for three shapes

Cross-sections that locate the majority of the material far from the bending axis have larger moments of inertia – it is more difficult to bend them. This is one of the reasons the I-beam is such a commonly used cross-section for structural applications – most of the material is located far from the bending axis, which makes it very efficient at resisting bending whilst using a minimal amount of material.

Area Moment of Inertia vs Second Moment of Area

Both the terms “second moment of area” and “area moment of inertia” are used. Second moment of area is often preferred to avoid any confusion with the moment of inertia, which is a completely different parameter that describes the resistance of a body to angular acceleration, although it is calculated in a similar way.

How to calculate the area moment of inertia

For any arbitrary cross-section like the one shown in the image below, the area moment of inertia can be calculated using this equation:

Area Moment of inertia
$$I_x = \int{y^2 dA}$$ $$I_y = \int{x^2 dA}$$

The $x$ and $y$ subscripts indicate that the area moment of inertia is for for bending about the $x$ and $y$ axes respectively.

The equations above can be used to calculate $I$ for any arbitrary shape

Let’s look an example of how this equation can be applied to calculate $I$ for a rectangular cross-section.

Example - Rectangular Cross-Section

We will use the equation shown above to calculate $I$ for bending about the $x$ axis for the following cross-section:

We can think of this rectangular cross-section as being made up of a large number of very thin strips that have a width $b$ and a height $dy$.

The area of one strip is:

$$dA = b \cdot dy$$

$I_x$ is given by the following equation:

$$I_x = \int{y^2 dA}$$

Subtituting in the equation for $dA$:

$$I_x = \int{by^2 dy}$$

Each strip contributes to the area moment of inertia. This is why we are integrating – to calculate the effect of all of these really small strips. Because the $y$ term is squared, the strips further away from the bending axis (the $x$ axis) contribute much more to $I$ than those close to the axis. To calculate $I_x$ all we have to do is integrate from the bottom of the rectangle at $y = -h/2$ to the top of the rectangle at $y = h/2$.

$$I_x = b\left[ \frac{y^3}{3} \right ]_{-h/2}^{h/2}$$ $$I_x = \frac{bh^3}{12}$$ This gives us the equation for $I_x$. If we repeat the process for bending about the $y$ axis instead, we get the following equation: $$I_y = \frac{b^3h}{12}$$

Fortunately you don’t have to go through this process of integrating whenever you need to figure out $I$ for a cross-section and bending axis. If it’s a fairly standard shape you can just look up an equation that has already been derived for your particular cross-section. Most strength of materials textbooks include tables like the one shown below that list $I$ equations for common cross-sections. You can use our area moment of inertia calculator to calculate area moment of inertia values for different cross-sections.

Cross-SectionArea Moment of Inertia
Filled Circle
$$I_x = I_y = \frac{\pi}{4}r^4$$
Hollow Circle
$$I_x = I_y = \frac{\pi}{4}(r_2^4 – r_1^4)$$
Rectangle
$$I_x = \frac{bh^3}{12}$$$$I_y = \frac{b^3h}{12}$$

The Parallel Axis Theorem

The parallel axis theorem is a really useful theorem that makes it easy to calculate $I$ for different bending axes without having to derive the equation from scratch using the integration method.

Parallel Axis Theorem
$$I_x = I_{xc} + Ad^2$$

It states that the area moment of inertia about any axis $I_x$ can be calculated from the area moment of inertia about a parallel axis $I_{xc}$ that passes through the centroid of the cross-section, the area of the cross-section $A$ and the distance between the two axes $d$.

Illustration of the parallel axis theorem, which can be used to calculate $I_x$ based on $I_{xc}$, $d$ and the cross-section area $A$. C is the centroid of the cross-section.

The centroid is the geometric center of the cross-section, or in other words the point at which you would be able to balance the cross-section on a pin.

Reference texts normally provide equations for $I$ for centroidal axes, so the parallel axis theorem is a powerful tool for extending those equations to any other parallel axes.

Adding and Subtracting Area Moments of Inertia

Area moments of inertia can be summed and subtracted to calculate values for composite cross-sections. The image below shows how this technique can be used to calculate $I_x$ for a hollow section.

An example of calculating $I$ for a composite cross-section by adding or subtracting

When using this method you need to make sure that the $I$ values for the component cross-sections ($I_{xA}$ and $I_{xB}$ in the example above) correspond to the correct bending axis, or else you will first need to apply the parallel axis theorem to get $I$ values for the correct axis.

Applications of the Area Moment of Inertia

The area moment of inertia is an important parameter for any application that which involves bending of a structural member, which means it appears constantly in the analysis of beams and columns.

Here are a few examples.

Beam Deflection

$I$ appears in the equation that is used to determine the deflection of a beam for an applied bending moment M.

$$\frac{d^2 v}{dx^2}= \frac{M}{EI}$$
Column critical buckling load

$I$ appears in the equation that gives the critical load at which a column will buckle.

$$P_{cr} = \frac{\pi^2 E I}{L^2}$$

If you’re interested in learning more about these applications, check out the beam deflection and buckling pages.

As demonstrated by the two examples shown above, the area moment of inertia often appears in equations alongside Young’s modulus $E$. The term $EI$ is given the name flexural rigidity. $I$ represents the stiffness of a beam cross-section due to its geometry, and $E$ represents the stiffness of the cross-section due to its material. The flexural rigidity $EI$ represents the total stiffness of the cross-section.

Polar Moment of Inertia

In addition to calculating the area moment of inertia for $x$ and $y$ axes that are in the same plane as the cross-section, we can also calculate the area moment of inertia for an axis that is perpendicular to the cross-section. This is called the polar moment of inertia, and it is usually denoted either using the letter $J$ or as $I_z$. It is often used in problems involving torsional deformation, which is the twisting of a beam or shaft.

Polar Moment of Inertia
$$J = \int{\rho^2 dA}$$

$J$ accounts for how the area of the cross-section is distributed radially relative to the rotation or twisting axis $z$. The $\rho$ term is the distance from the $z$ axis (which is pointing out of the screen in the image below) to an element dA.

The polar moment of inertia is calculated based on the distribution of the area of the cross-section relative to a twisting axis ($z$ in the image above)

Like with $I_x$ and $I_y$, the $\rho$ term is squared in the equation, which means that areas of the cross-section that are located far from the axis of rotation contribute most to the value of $J$. This is why transmission shafts are hollow – the central portion of the cross section doesn’t contribute much to the torsional resistance, so it’s more efficient to use hollow shafts.

An interesting observation we can make is that the polar moment of inertia about an axis passing through a specific point on the cross-section is equal to the sum of the area moments of inertia for two perpendicular axes that pass through the same point. This is called the perpendicular axis theorem.

Perpendicular Axis Theorem
$$J = I_x + I_y$$

The derivation for this theorem is pretty simple – check out the Understanding the Area Moment of Inertia video if you’d like to see it.

Releated Topics

Trusses

Trusses are structures (e.g bridges or roofs) made up of members that can only carry tensile or compressive axial loads.

Stress and Strain

Stress and strain are fundamental concepts that relate to the internal forces and deformations within a body in response to applied loads.

Understanding the Area Moment of Inertia Read More »

Understanding True Stress and True Strain

In a typical stress-strain curve, stress is defined as the applied force divided by the original cross-sectional area of the test specimen, and strain is defined as the change in specimen length divided by the original length. But these are just approximations of the stress and strain in the specimen. They are called engineering stress and engineering strain.

True stress and true strain are the actual stress and strain in the specimen, that account for the fact that the dimensions of the specimen change throughout the duration of the test. The video below explores the topic of true stress and true strain in more detail.

Understanding True Stress and True Strain Read More »

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