FEXLA

Why every nozzle check is also run with the pressure off

Pressure tension can cancel load compression, so the load alone can govern. The cases FEXLA runs with pressure at zero.

FEXLA engineering · · 5 min read

Shell model of a cylinder with a padded nozzle, pressure arrows on every wall and a force and a moment at the nozzle end
Fig. 1 · Shell model of a cylinder with a padded nozzle, pressure arrows on every wall and a force and a moment at the nozzle end

Internal pressure puts the shell in tension, and that tension can cancel part of the compression a nozzle load causes. With the pressure off, the load's stress stands alone and can be the larger, so ASME Section VIII Division 1, Appendix 46-4(c)(1) asks for cases with the pressure equal to zero as well.

The shell model in FEXLA adds those cases by itself. In the WRC 537 calculator today it is a second run, and this post shows why it is worth doing.

Pressure and load stresses have signs

Internal pressure gives membrane tension in the shell, hoop and longitudinal, at every point. The stresses from nozzle loads have both signs. A moment puts tension on one side of the nozzle and compression on the other. Bending puts tension on one face of the wall and compression on the other. A radial load that pushes the nozzle into the shell puts the shell round it into membrane compression.

The loads at an attachmentA section through a curved shell with a nozzle standing on it. Arrows show a radial force along the nozzle, a shear across its end, a bending moment as a curved arrow, and torsion as an arrow circling the nozzle. The patch of shell round the nozzle base is shaded.Radial force (push or pull)Sheartwo directionsBendingmomenttwo directionsTorsionAll of it enters the shell through the shaded patch
Figure 2. The six loads at a nozzle. Each gives tension at some points of the shell and compression at others.

Where a load stress is tensile, pressure adds to it and the case with pressure is the worse one. Where it is compressive, pressure takes away from it, and the case without pressure can be the worse one. The point that governs, and the check that governs, can change between the two.

Stress contour on a FEXLA shell model of a nozzle on a cylinder
Figure 3. Stress contour on a shell model of a nozzle: the stress gathers round the junction and dies away within a short distance along the shell.

One point, with and without pressure

The same load is four times as severe without the pressure. On the far side of a moment the opposite holds: load tension adds to pressure tension, and the case with pressure governs. Neither case is always the worse one, so both are run and the worse governs at each point.

A vessel does spend time like this. At shutdown or before it is pressurised, the weight of the connected line still hangs on the nozzle. A check made only at design pressure has assumed that the pressure is always there to help.

What the code asks

Division 1 has no rules of its own for local loads. Through U-2(g) and Mandatory Appendix 46 it uses the design-by-analysis rules of Division 2, Part 5 with the Division 1 allowable stress. Appendix 46-4(c)(1) adds cases with the pressure equal to zero to the load combinations. Appendix 46-4(b) also says the 1.2 increase for wind or earthquake, a design-by-rule allowance, does not apply.

What the shell model runs

The shell model is linear. Pressure is solved once as its own basic case, so a combination without it costs nothing more than an addition. It adds a zero-pressure twin to every combination that has both a pressure and a load:

CaseWhat is in itAdded whenChecked as
SUS0Weight D, with P = 0There is weight and a design pressurePrimary
OCC0D plus wind or earthquake, with P = 0There is an occasional row and a pressure acting with itPrimary
OCCL0D plus 0.75 × occasional plus 0.75 × operating, with P = 0As OCC0, with load-controlled operating loadsPrimary
OPE0D plus operating loads and thermal state, with P = 0There are operating or thermal loads and an operating pressureRange from shutdown against SPS
The zero-pressure cases. With the reversal options on, they also run with the occasional row reversed.

The range from shutdown matters as much as the primary checks. Where the operating loads give compressive stress, the range to the operating state without pressure can be the larger, so OPE0 can govern the primary plus secondary check.

The other analyses follow the same rule. Limit load runs its combinations with the pressure not acting as well. Buckling runs each combination with the pressure not acting, since internal pressure's tension also offsets the compression that buckles a shell.

In the WRC 537 calculator

The calculator checks one load set at the design pressure entered. It adds the pressure stress at every point, raised at the nozzle edge by the pressure stress intensity factor of Division 2, 4.5.5. It does not add a zero-pressure case by itself.

  • Run the job a second time with the design pressure set to zero, and keep both reports. With no pressure, the pressure term and its intensity factor drop out, and the load stresses stand alone.
  • The option to run the radial load reversed as well changes the sign of that load only. It is not a zero-pressure case.
  • The calculator's own validation includes such zero-pressure cases, called hot shut-down, because they isolate the load stresses.

Where it stops

  1. 01In the WRC 537 calculator the zero-pressure case is a second run by the engineer; it is not added automatically.
  2. 02The shell model adds a zero-pressure case only where there is both a pressure and a load to pair it with.
  3. 03Vacuum and external pressure are a different case: there the pressure itself compresses the shell. This post is about internal pressure.
  4. 04The finite-element results are early access and under verification.
B-30

Try it in FEXLA

The Nozzle loads card runs the WRC 537 check at the pressure you enter, and the shell model with its zero-pressure cases added.

Open the card

References

  • ASME Section VIII Division 1, U-2(g); Mandatory Appendix 46, 46-4(b) and 46-4(c)(1).
  • ASME Section VIII Division 2, Part 5, Table 5.3; 4.5.5 (pressure stress intensity at a nozzle).
  • WRC Bulletin 537.

Method notes this draws on

Next post: How long should the shell be around a nozzle

Educational article. It explains principles and is not design guidance; follow your governing code and edition.