Axially loaded members
A crane cable, a bridge hanger, a bolt clamping two steel plates — all of them are, mechanically, the same simple object: a slender member carrying force purely along its own length. No bending, no twisting, just a straight pull or push from end to end. Yet this simplest of loadings hides real design subtlety the moment a member is built from several segments, restrained at both ends so it cannot freely expand, or heated. This article takes the single relation linking stress, strain and Hooke's law — — and extends it three ways: to members with several segments of different force, area or material; to statically indeterminate bars, where equilibrium alone cannot find the reactions and a compatibility condition is needed; and to thermal effects, where a restrained member can develop serious stress from nothing more than a change in temperature. Two fully worked numerical examples, reused and extended from the shorter version of this topic, anchor every idea in a concrete calculation.
For a prismatic bar under constant internal axial force, elongation follows ; multi-segment members use superposition of this formula segment by segment, statically indeterminate bars need an added compatibility equation beyond equilibrium, and a restrained member develops thermal stress precisely because it is prevented from executing its free thermal deformation .
The core idea
From three basic laws to one formula. A prismatic bar of length , cross-sectional area and elastic modulus , carrying a constant internal axial force , obeys three relations you already know: the definition of normal stress , the definition of normal strain , and Hooke's law . Combine them — — and rearrange to get the axial-deformation formula that anchors this whole unit:
where: is the axial elongation (positive) or shortening (negative), is the internal axial force (positive in tension), is the member length, is the cross-sectional area, and is Young's modulus. The product is the member's axial stiffness — the larger it is, the less a given and deform the bar, exactly the way a stiffer spring stretches less under the same load.
Superposition for varying , , or . Real members are rarely one uniform segment end to end. A stepped shaft changes cross-section; a bar loaded at an intermediate point carries different internal force on either side of that point; a composite bar may splice two materials. In every such case, split the member into segments over which , , and are each individually constant, find the internal force in each segment by sectioning and equilibrium (not simply the externally applied load), compute for each, and sum algebraically:
Elongations and shortenings carry opposite signs in this sum, so a segment in compression subtracts from one in tension.
Statically indeterminate axial members. When a bar is fixed at both ends (or otherwise over-restrained) and loaded partway along, there are more unknown reactions than independent equilibrium equations, and equilibrium alone cannot solve for them. The missing equation comes from a compatibility condition — a geometric statement about how the deformations of the parts must fit together. For a bar rigidly fixed at both ends, the total elongation from one fixed end to the other must equal zero, because the fixed points cannot move. The solution method has three parts: write the equilibrium equation(s); write the compatibility equation by expressing each segment's deformation as in terms of the unknown reactions, and set the sum equal to the known geometric constraint; then solve the two equations simultaneously.
Thermal strain and stress. A free, unrestrained member subjected to a uniform temperature change develops a thermal strain
where: is the material's coefficient of thermal expansion (per degree) and is the temperature change. This produces a free thermal deformation with zero stress, because nothing is resisting the expansion. If instead the member is restrained — for example fixed rigidly between two walls — it cannot execute this free deformation, and the restraint forces a thermal stress to develop. Such problems are solved exactly like mechanical indeterminate problems: write equilibrium, then a compatibility equation that now contains both a mechanical term and a thermal term , set to match the physical constraint (typically total deformation equals zero for full restraint).
Why superposition and compatibility work together
Rather than a single formula derivation, the reasoning that unlocks every indeterminate or multi-segment axial problem is a fixed three-part logic, and it is worth stating in full because the same structure recurs across statics-of-deformable-bodies problems well beyond this course: the number of independent equations you can write must equal the number of unknowns you are solving for, and when equilibrium alone falls short by exactly the "degree of indeterminacy," compatibility supplies precisely that many extra equations, no more and no less.
Step 1. Count unknowns and equilibrium equations. For a bar with reactions at both fixed ends and one intermediate load, there are two unknown reactions (, ) but only one independent equilibrium equation along the bar's axis (sum of axial forces equals zero). The shortfall is one equation — the bar is indeterminate to the first degree.
Step 2. Section the bar into segments carrying known internal force in terms of the unknowns. Cutting on either side of the load point shows one segment carries and the other carries (with sign convention for tension positive), each segment's internal force found from a free-body diagram of the portion cut away, not from guessing.
Step 3. Translate the physical restraint into a deformation statement. Because both ends are rigidly fixed, the total distance between them cannot change: the sum of the two segments' elongations, computed from using the internal forces from Step 2, must equal zero. This is the compatibility equation — it says nothing about forces directly, only about geometry, which is exactly why it supplies genuinely new information beyond equilibrium.
Step 4. Solve the equilibrium and compatibility equations together as a simultaneous system in the unknown reactions. Once the reactions are known, every segment's internal force, stress, and elongation follow directly from the earlier formulas — the indeterminate problem collapses back into an ordinary determinate calculation once the extra unknown is pinned down.
Worked example
A stepped steel bar ( GPa) has two segments in series: AB is m long with area mm², and BC is m long with area mm². A tensile axial force of kN acts at the free end C, with the bar fixed at A. Find the total elongation, then extend the same bar to the indeterminate case.
Step 1. Find the internal force in each segment. Since the only load is the kN tension at C and the bar is otherwise unloaded between A and C, both segments carry the full internal force kN in tension — sectioning anywhere along either segment and summing forces on the cut piece confirms this.
Step 2. Compute . With and m,
Step 3. Compute . With and m,
Step 4. Sum by superposition. .
Competitive stretch
Now suppose instead the same m total bar (uniform mm², so the stepped geometry is replaced by a single material and section for this variant) is fixed rigidly at both ends A and C, with a tensile force kN applied at an intermediate point B located m from A. Let , be the tensile reactions at the two fixed ends. Equilibrium at B gives kN — one equation, two unknowns, indeterminate to the first degree. Compatibility (total elongation A to C is zero) gives, after cancel since they are uniform, , so . Substituting: kN and kN. Checking, ✓, confirming compatibility is satisfied. The reactions are kN and kN.
Common traps
- Using the external applied load directly in for each segment instead of the correct internal force in that segment found by sectioning — these differ whenever loads are applied at intermediate points.
- In indeterminate problems, trying to solve two unknown reactions from one equilibrium equation alone, forgetting that a compatibility equation is required to close the system.
- Sign errors in the compatibility equation — elongation and shortening must be assigned consistent signs so the geometric constraint (e.g. total elongation equals zero) is written correctly.
- For thermal problems, forgetting that a free member under develops strain but no stress; thermal stress only arises when deformation is restrained, and the compatibility equation must then combine both mechanical and thermal deformation terms.
Ask the tutor: If you get stuck writing the compatibility equation for a statically indeterminate bar, or want to check your sign convention on a thermal-stress problem, ask the AI tutor to walk through the free-body diagrams step by step.
Why does the internal force sometimes differ from the applied load in a multi-segment bar?
Because internal force is whatever force is transmitted across a given cross-section, which you find by cutting the bar at that section and applying equilibrium to one side — not by reading off the external load directly. If a load is applied only at the free end with nothing in between, every segment does carry that same force. But once an intermediate load is applied partway along the bar, sectioning on either side of that point gives different internal forces, so each segment's must use its own sectioned value.
How do I know how many compatibility equations an indeterminate problem needs?
Count unknown reactions, subtract the number of independent equilibrium equations available (for a purely axial bar along one line, that is just one: sum of axial forces equals zero), and the result is the degree of indeterminacy — exactly the number of compatibility equations you must write. A bar fixed at both ends with one intermediate load is indeterminate to the first degree, needing exactly one compatibility statement, typically that the total elongation between the fixed ends is zero.
Why does a restrained bar develop thermal stress even though nothing external is pushing on it?
Because the restraint itself acts like an external constraint force. A free bar under would simply grow by with no resistance and hence no stress. When the ends are fixed, that growth is physically prevented, so the walls must push back with an internal axial force large enough to cancel the free thermal deformation exactly; that internal force, divided by area, is the thermal stress. It is set up with the same compatibility logic as a mechanical indeterminate problem, just with an added term in the deformation equation.