Truss analysis by the method of joints finds the force in each member by balancing forces at one joint at a time. In the standard statics model, the truss is planar, members are pin-connected two-force members, and external loads act only at the joints. Under those conditions, each joint must satisfy

Fx=0,Fy=0\sum F_x = 0, \qquad \sum F_y = 0

where Fx\sum F_x is the sum of horizontal force components at a joint and Fy\sum F_y is the sum of vertical force components.

Why The Two Equations Are Enough

The method works because of what a "two-force member" means. Each truss member is pinned at both ends and loaded only at those ends, so the only way it can stay in equilibrium is to carry force purely along its own length. It cannot resist bending at the joints the way a beam or rigid frame would.

That single fact is what lets you reduce the whole structure to small problems. At a single joint in a planar truss, every member force passes through that point, so there are no moment arms and the moment equation gives nothing new. You are left with exactly two independent equations per joint. As long as a joint has at most two unknown member forces, those two equations solve it completely, which is why you always look for such a joint to start.

Formula And Symbols

For each joint you resolve angled member forces into horizontal and vertical components, then apply:

Fx=0,Fy=0\sum F_x = 0, \qquad \sum F_y = 0

A practical convention is to assume each unknown member force is tensile at the start. If a solved force comes out negative, the member is actually in compression. Physically, a member that pushes on a joint is in compression, and one that pulls on a joint is in tension.

Worked Example: A Simple Triangular Truss

Consider a symmetric triangular truss with supports at joints AA and CC, a top joint BB, and a downward load of 10 kN10\ \mathrm{kN} at BB. Let AA be a pin support, CC a roller support, and let members ABAB and BCBC each make a 4545^\circ angle with the horizontal bottom member ACAC.

Because the load is centered, symmetry gives the support reactions

Ay=5 kN,Cy=5 kNA_y = 5\ \mathrm{kN}, \qquad C_y = 5\ \mathrm{kN}

and Ax=0A_x = 0.

Now start at joint BB. Only two member forces are unknown there, and symmetry says they have the same magnitude. Call that magnitude FF. At joint BB, the vertical components of the two inclined members must balance the 10 kN10\ \mathrm{kN} downward load:

2Fsin45=102F \sin 45^\circ = 10

so

F=102sin45=102(0.707)7.07 kNF = \frac{10}{2 \sin 45^\circ} = \frac{10}{2(0.707)} \approx 7.07\ \mathrm{kN}

To hold up joint BB, the inclined members must push on it, so ABAB and BCBC are in compression, each with magnitude 7.07 kN7.07\ \mathrm{kN}.

Next move to joint AA. The compressive force in ABAB has a horizontal component of

7.07cos45=5 kN7.07 \cos 45^\circ = 5\ \mathrm{kN}

At joint AA, that horizontal component must be balanced by member ACAC, so

FAC=5 kNF_{AC} = 5\ \mathrm{kN}

Because ACAC pulls on the joint, it is in tension. The member forces are:

FAB=FBC=7.07 kN (compression),FAC=5 kN (tension)F_{AB} = F_{BC} = 7.07\ \mathrm{kN}\ \text{(compression)}, \qquad F_{AC} = 5\ \mathrm{kN}\ \text{(tension)}

Practice The Same Method

Keep the same truss geometry, but change the top load from 10 kN10\ \mathrm{kN} to 14 kN14\ \mathrm{kN}. Because the geometry stays the same and the model is still linear statics, each member force scales by the same factor: FAB=FBC9.9 kNF_{AB} = F_{BC} \approx 9.9\ \mathrm{kN} in compression and FAC=7 kNF_{AC} = 7\ \mathrm{kN} in tension. Check your scaling by recomputing 2Fsin45=142F\sin 45^\circ = 14 directly. For a harder case, set up a truss that is not symmetric and decide which joint becomes solvable first after you compute the support reactions.

Calculation Traps To Watch

The most common mistake is starting at a joint with too many unknowns. In a planar truss, each joint gives only two independent equilibrium equations, so a joint with three unknown member forces usually cannot be solved first.

Another mistake is skipping the support reactions. If the reactions are wrong, every member force that follows will also be wrong.

Students also misread negative answers. With a consistent sign convention, a negative force usually means the member is in the opposite state from the one you assumed at the start.

The last big trap is using the method on a structure that is not modeled as a truss. The assumptions matter: the method works when joints are modeled as pins, loads and reactions are applied at joints, and the truss is in static equilibrium. Beams and rigid frames can carry bending moments, so they need a different analysis.

Where The Method Of Joints Is Used

The method of joints appears often in statics courses because it teaches how loads move through a structure. It is also useful for hand-checks of simple roof trusses, bridges, and other pin-jointed systems. In more complex engineering work, software usually analyzes the full structure, but this method still builds intuition about load paths and member-force signs.

Frequently Asked Questions

What assumptions does the method of joints make?
In the standard statics model, the truss is planar, members are pin-connected two-force members, and external loads act only at the joints. Each member carries force only along its own length and does not resist bending at the joints the way a beam or rigid frame would. The truss must also be in static equilibrium for the joint equations to apply.
How do you solve a truss using the method of joints?
First find the support reactions from whole-truss equilibrium. Then pick a joint with at most two unknown member forces, resolve angled forces into components, and apply the two force-balance equations at that joint. Move to the next solvable joint and repeat. Instead of solving the whole structure at once, you break it into small equilibrium problems solved joint by joint.
How do you tell if a truss member is in tension or compression?
A common approach is to assume each unknown member force is tensile at the start. If a solved force comes out negative, the member is actually in compression. Physically, a member that pushes on a joint is in compression, while one that pulls on the joint is in tension, as with the inclined members versus the bottom chord in a simple triangular truss.
When does the method of joints not apply?
The assumptions matter. If a member carries distributed load along its length, or if the structure behaves like a rigid frame where joints transfer bending, the method of joints by itself is not the right model. It works when joints are modeled as pins, loads and reactions are applied at joints, and the truss is in static equilibrium.

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