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Allowable Stress by Material

Calculate design allowable stress per ASME VIII Div.1 or EN 13445-3. Temperature-dependent properties, creep rupture check, weld joint efficiency factor. 12+ material grades.

ASME VIIIEN 13445σ_allowCreep CheckWeld Factor
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Design Allowable Stress

Allowable Stress σ_allow × E
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Rp0.2(T) / Safety Factor
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Rm(20°C) / Safety Factor
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σ_allow (before weld factor)
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Governing Criterion
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Creep Range Check
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Load-Adjusted Allowable
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Material Properties at T
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EN 13445-3 (Ferritic Steels)

ASME VIII Div.1

Temperature Derating

Both yield and UTS decrease with temperature. This calculator uses linearized derating curves based on EN 10028 / ASME II-D data:

  • Below 100°C: properties are at room-temperature values
  • 100–400°C: gradual reduction (yield drops faster than UTS)
  • Above 400°C: significant reduction; creep may govern

Creep Regime

When the design temperature exceeds the creep onset temperature, time-dependent rupture stress governs. Typical creep onset:

Material TypeCreep Onset (°C)Typical Max Design T
Carbon steel (S235, S355)~350400°C
C-Mn pressure (P265GH, P355GH)~380450°C
Mo steel (16Mo3)~400500°C
CrMo steel (13CrMo4-5)~450550°C
2¼Cr-1Mo (10CrMo9-10)~470600°C
Austenitic SS (304, 316L)~500700°C

Practical Example

Example — P265GH at 250°C, EN 13445

Given: P265GH, Rp(20)=265 MPa, Rm=410 MPa, T=250°C, weld E=1.0

Rp(250°C) ≈ 265 × 0.85 = 225.3 MPa (derating for temperature)

f_yield = 225.3 / 1.5 = 150.2 MPa

f_UTS = 410 / 2.4 = 170.8 MPa

f = min(150.2, 170.8) = 150.2 MPa (yield governs)

With E=1.0: σ_allow = 150.2 MPa

Material Comparison at Room Temperature

MaterialRp0.2Rmf (EN)S (ASME)
S235JR235360150103
S355JR355510213146
P265GH265410171117
P355GH355490204140
16Mo3280450187129
13CrMo4-5295460192131
10CrMo9-10275450183129
304 SS210520140138
316L SS200500133133
2205 Duplex450620258177

⚠️ Note: This calculator provides approximate values for preliminary design. Always verify with the actual code tables (ASME II-D, EN 10028, EN 10222) for your specific material grade, product form, thickness, and temperature.

Allowable stress is the maximum stress permitted in a design component. It is the material strength divided by a code-defined safety factor. Using it ensures the component won’t fail under normal (or abnormal) loading with an adequate safety margin.

Different codes use different safety factors, leading to different allowable stresses for the same material.

ASME VIII uses a UTS safety factor of 3.5 (was 4.0 before 2007), while EN 13445 uses 2.4. This means ASME is more conservative on the UTS criterion. However, both use 1.5 on yield.

For high-strength materials where yield governs (e.g. S355, 2205), both codes give similar results. For lower-strength materials where UTS governs, ASME is significantly more conservative.

Both yield strength and UTS decrease with temperature. The yield strength decreases faster. Above the creep onset temperature, time-dependent rupture stress may become the governing criterion.

Example: S355 at 400°C has Rp ≈ 297 MPa (vs 355 at RT), so allowable drops from 213 to ~173 MPa (EN).

Creep is significant above: ~350°C for carbon steel, ~400°C for Mo steel, ~450°C for CrMo, ~500°C for austenitic SS. Above these temperatures, the 100,000h creep rupture stress divided by its safety factor may be lower than the yield-based allowable.

Weld joint efficiency (E or z) accounts for potential weld defects:

  • E=1.0: Full radiographic or ultrasonic examination of all welds
  • E=0.85: Spot (partial) radiographic examination
  • E=0.7: No volumetric NDE (visual only)

The effective allowable = σ_allow × E. Using E=1.0 requires more NDE but allows thinner walls.

The procedures described on this page were developed and field-tested by the Vibromera team using the Balanset-1A, a portable dual-channel balancer and vibration analyzer for on-site rotor balancing.

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