MULTICALCI
ASME VIII Div 1 · UG-27 shells · UG-32 heads

Pressure Vessel Thickness Calculator

Required wall thickness for cylindrical shells, spherical shells, hemispherical heads and 2:1 ellipsoidal heads under internal pressure. Returns nominal plate thickness, hoop and longitudinal stress in the corroded condition, and maximum allowable working pressure.

ASME VIII Div 1 UG-27(c)(1) UG-32(d)/(f) UW-12 joint efficiency

Calculate required thickness

Design Conditions
Set automatically by material.

Enter your values and select Calculate.

ASME VIII thickness formulas

All four cases use the thin-shell membrane equations of ASME Section VIII Division 1. The corrosion allowance is added after the pressure calculation, and stress and MAWP are then checked on the corroded thickness — the condition the vessel must still be safe in at the end of its life.

— Required thickness under internal pressure — Cylindrical shell t = P·R / (S·E − 0.6P) UG-27(c)(1) Spherical shell t = P·R / (2·S·E − 0.2P) UG-27(d) Hemispherical head t = P·R / (2·S·E − 0.2P) UG-32(f) 2:1 ellipsoidal head t = P·D / (2·S·E − 0.2P) UG-32(d) tgross = t + CA tnominal = round up tgross to the next 0.5 mm tnet = tnominal − CA — corroded wall — Checked on the corroded wall — σh = P·R / tnet — hoop stress (cylinder) σl = P·R / (2·tnet) — longitudinal stress MAWP = S·E·tnet / (R + 0.6·tnet) — cylinder

P internal design pressure (MPa) · R inside radius (mm) · D inside diameter (mm) · S maximum allowable stress (MPa) · E joint efficiency · CA corrosion allowance (mm) · tnet corroded thickness (mm)

On the margin figure. The ratio reported as safety factor is S·E ÷ σh — margin against the code allowable stress, not against burst. S already contains the code's own safety factor against ultimate tensile strength, so a value just above 1.0 is normal and means the plate chosen is close to the minimum required.

Worked example

A carbon steel cylindrical vessel, 1500 mm inside diameter, designed for 10 bar at 150 °C, spot radiographed, with 3 mm corrosion allowance.

Given
Component
Cylindrical shell
Design pressure P
10 bar = 1.0 MPa
Inside diameter D
1500 mm → R = 750 mm
Allowable stress S
138 MPa (carbon steel)
Joint efficiency E
0.85 (spot radiography)
Corrosion allowance
3 mm
Step 1 — required thickness
S·E = 138 × 0.85
117.3 MPa
t = 1.0 × 750 / (117.3 − 0.6)
6.427 mm
Step 2 — plate selection
tgross = 6.427 + 3
9.427 mm
Round up to next 0.5 mm
9.5 mm nominal
tnet = 9.5 − 3
6.5 mm corroded
Step 3 — corroded-condition check
σh = 1.0 × 750 / 6.5
115.38 MPa
σl = σh / 2
57.69 MPa
MAWP = 117.3 × 6.5 / (750 + 3.9)
1.011 MPa = 10.11 bar
Margin = 117.3 / 115.38
1.017
9.5 mm plate · σh 115.38 MPa vs 117.3 allowable · MAWP 10.11 bar

The vessel is adequate but tight — MAWP exceeds design pressure by only 1 %. Moving to full radiography (E = 1.00) would drop the required thickness to 5.46 mm and allow the same 9.5 mm plate to carry a considerably higher MAWP, which is often worth the inspection cost.

Units and input ranges

QuantitySymbolUnitAccepted range
Design pressurePbar, MPa or psi> 0
Inside diameterDmm or in> 0
Allowable stressSMPa> 0
Joint efficiencyEdimensionless0.1 – 1.0
Corrosion allowanceCAmm≥ 0
Design temperatureT°C or °Fany
Required thicknesstmmoutput
Nominal platetnominalmmoutput
MAWPbaroutput

Pressure is converted to MPa internally: 1 bar = 0.1 MPa and 1 psi = 0.00689476 MPa. Diameters in inches are converted at 25.4 mm. The ASME minimum shell thickness of 1.5875 mm (1/16 in) is applied as a floor.

Joint efficiency — ASME VIII Div 1 Table UW-12

ExaminationEEffect on thickness
Full radiography1.00Thinnest plate, highest inspection cost
Spot radiography0.85Common compromise
No radiography0.70Roughly 43 % more plate than full RT

Allowable stress at ambient

MaterialS (MPa)Typical use
Carbon steel138General pressure vessel plate
Stainless 304138Corrosion service, food and pharma
Stainless 316115Chloride and acid service
Temperature derating. These are ambient values. Allowable stress falls with temperature, and above about 50 °C you should take S from ASME Section II Part D Table 1A for the actual design temperature rather than relying on the ambient figure.

Frequently asked questions

How is pressure vessel wall thickness calculated?

For a cylindrical shell under internal pressure ASME Section VIII Division 1 paragraph UG-27 gives t = P·R / (S·E − 0.6P), where P is internal design pressure, R is the inside radius, S is the maximum allowable stress and E is the joint efficiency. The corrosion allowance is added afterwards, and the result is rounded up to an available plate thickness.

What is joint efficiency E in ASME VIII?

Joint efficiency accounts for the reliability of welded seams and the extent of radiographic examination. Under ASME Section VIII Division 1 Table UW-12 a double-welded butt joint with full radiography takes 1.00, with spot radiography 0.85, and with no radiography 0.70. Lower joint efficiency directly increases the required thickness, so the cost of radiography is often offset by the saving in plate.

How much corrosion allowance should a pressure vessel have?

Typical corrosion allowance is 1.5 to 3 mm for carbon steel in general service, and 3 to 6 mm in corrosive duty. Stainless steel and clad vessels often carry zero or a nominal allowance. The allowance is added to the calculated thickness before rounding up to plate size, and it is subtracted again when checking stress and maximum allowable working pressure in the fully corroded condition.

What is MAWP and how does it differ from design pressure?

Maximum allowable working pressure is the highest pressure the vessel may carry in its corroded condition at design temperature, based on the thickness actually installed. Design pressure is the value the vessel was specified to. Because nominal plate is always thicker than the calculated requirement, MAWP is normally somewhat higher than design pressure, and it is MAWP that sets the relief valve pressure.

When do the thin-wall formulas stop being valid?

The UG-27 membrane formulas assume a thin shell where stress is essentially uniform through the wall. They apply while thickness does not exceed half the inside radius, or equivalently while pressure does not exceed 0.385·S·E. Beyond that the through-wall stress gradient becomes significant and the thick-wall rules of ASME Section VIII Division 1 Appendix 1-2 or Division 2 must be used instead.

Related mechanical calculators

← All mechanical engineering calculators