The Bree diagram is a chart of steady primary stress against cycling thermal stress, both divided by yield, that shows whether a thin cylinder stays elastic, shakes down, cycles plastically or ratchets. It comes from a closed-form analysis of one idealised case: a thin tube under steady internal pressure with a temperature difference through its wall that comes and goes. Design rules use two of its boundaries as limits on the thermal stress range a given pressure stress allows.
The article on ratcheting and shakedown explains the four outcomes in general. This one goes into the cylinder itself, the two stresses that set its place on the chart, and why each region behaves as it does.

The cylinder behind the chart
Take a long, thin cylinder far from its ends, so that nothing but pressure and temperature acts on the wall. The metal is idealised as elastic-perfectly plastic: it follows a straight line up to yield and then flows at constant stress. Yield is taken as the same hot and cold.
Inside, a steady pressure P sets up a membrane stress that is the same through the whole wall and never goes away. On top of it, each operating cycle heats the inside face more than the outside, with a temperature difference ΔT that varies linearly through the wall. At shut-down the difference goes back to zero, while the pressure stays.
The hot inside wants to grow more than the cooler outside. The wall cannot curl, because the cylinder is closed round on itself, so the gradient is held flat. The result is a bending stress through the wall: compression on the hot face, tension on the cool face, zero at mid-thickness. It is self-limiting, so it is a secondary stress.
Two stresses, two scales
The chart divides both by the yield stress. The horizontal scale is X = σp / Sy and the vertical scale is Y = σt / Sy, the range of the cycling thermal stress at the surface. A point on the chart is one pair of pressure and temperature cycle, and its region tells what the wall does after many cycles.
On the hot half of the cycle the two stresses add on the cool face and subtract on the hot one. On the cold half only the pressure stress is left. So the surface stress swings by σt on every cycle around a steady value σp.
The regions, one by one
- E, elastic: X + Y ≤ 1. The largest surface stress σp + σt never reaches yield, so nothing yields at all.
- S, shakedown: the first cycle yields a surface layer, the residual stress it leaves shifts later cycles into the elastic range, and the wall then cycles elastically. This needs Y ≤ 2, because an elastic swing can be at most twice yield.
- P, plastic cycling: Y above 2 but below 1/X. Both faces yield on every cycle, first one way and then the other, with no net growth. The wall does not distort, but each cycle spends low-cycle fatigue life.
- R1 and R2, ratcheting: to the right of Y = 4(1 − X) for X from 0.5 to 1, or above Y = 1/X for X up to 0.5. The wall stretches a little further on every cycle. In R1 an elastic core remains and the faces shake down; in R2 the faces also cycle plastically.
At X = 1 the pressure stress alone reaches yield across the wall. That is plastic collapse of the cylinder, with no thermal stress needed.
Why the wall grows each cycle
Ratcheting needs both stresses. When the cool face yields in tension on the hot half of the cycle, that layer can carry no more stress. The pressure still needs the same total force across the wall, so the elastic part has to carry more, and to do so it must stretch. On the cold half the thermal stress is removed, so its change runs the other way, the layer at the hot face yields in turn, and the same shift happens again. Each half cycle adds a little hoop strain, in the same direction every time, because the pressure always pulls the same way.
With a small pressure stress the elastic core is wide enough to carry the shifted load without yielding, which is why a large thermal range on its own only gives plastic cycling. As X rises, a smaller thermal range is enough to start the growth, so the boundary falls from Y = 2 toward zero at X = 1.
Placing a case on the chart
The example also shows how steep the change is. The temperature difference grows by less than a factor of two between case A and case B, but the outcome goes from a wall that settles after one cycle to one that grows on every cycle.
From boundaries to design limits
Design rules take two ideas from the chart. The first is the Y = 2 line: the range of primary plus secondary stress is limited to about twice yield, which in allowable-stress terms is often written as about 3 S. Keeping below it keeps the wall in the elastic or shakedown regions.
The second is a thermal stress ratcheting check that lowers the allowed thermal range as the steady stress rises, following Y = 1/X for X up to 0.5 and Y = 4(1 − X) above it. Design-by-analysis rules, including ASME Section VIII, Division 2, have a check of this kind. The stresses that go in, the yield value at which temperature, and the cases it applies to are code-specific, so check the governing code.
The chart has limits of its own. It assumes a thin wall, a linear temperature gradient, the same yield hot and cold, and no hardening. At a nozzle or a junction the stresses are not this simple, and an elastic-plastic analysis over several cycles is the more direct check.
Key points
- The Bree diagram comes from one idealised case: a thin cylinder with steady pressure and a cycling linear temperature difference through the wall.
- X is the pressure membrane stress over yield; Y is the thermal bending stress EαΔT/(2(1 − ν)) over yield.
- Below Y = 2 the wall can shake down; above it, it cycles plastically or ratchets.
- Ratcheting needs both stresses: the steady pressure pulls the same way while the thermal stress shifts load to the elastic core each cycle.
- Design rules turn the Y = 2 line and the ratcheting boundaries into range limits, with code-specific details.
Where this matters in practice
- Shells and nozzles with a hot fluid inside and frequent start-ups, where the through-wall temperature difference comes and goes.
- Nozzle and attachment junctions whose primary plus secondary range comes close to its limit.
- Heat exchanger shells and tubesheets that see thermal transients on top of steady pressure.
- Any check where the range limit is exceeded and the next step is a ratcheting assessment.
FEXLA's local check at a nozzle or clip compares the combined local stress with limits built from the allowable stress S. It does not run a cycle-by-cycle analysis.
See the nozzle checkRelated principles
- Ratcheting and shakedownWhat happens when a steady stress meets one that cycles: shakedown, plastic cycling or ratcheting.6 min read
- Thermal stress: free expansion and restraintHeat causes stress only when something stops the metal from growing: full, partial and through-wall restraint.5 min read
- Fatigue: from S-N curves to weld design curvesFrom the smooth-bar S-N curve to the welded joint: stress range, cycles, damage sums and weld design curves.6 min read
Next principle: Fatigue: from S-N curves to weld design curves
Educational article. It explains principles and is not design guidance; follow your governing code and edition.