Allowable stress and minimum shell course thickness for design and test conditions (BS EN 14015:2004, §9.1–9.2)
◉ BS EN 14015:2004 §9.1–9.2 STYLE CHECK · NOT A REGULATORY SUBMISSION TOOL
⚠ Indicative tool only, and structurally distinct from the existing API 650 and IS 803 Shell Design/Thickness calculators. EN 14015 fixes joint efficiency at 1,0 throughout (§9.1.4) — no material/radiography table needed — and its allowable stress is capped at 260 N/mm² regardless of material grade (§9.1.1). Its thickness formula also includes the internal design/test pressure directly, which the basic API 650 and IS 803 formulas don't. Verified directly against this edition's page images; the test-condition formula (Eq.4) deliberately excludes the corrosion allowance term that the design-condition formula (Eq.3) includes, per the standard's own equations.
Identification
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Allowable Design & Test Stress (§9.1.1)
S = 2/3 × yield, capped at 260 N/mm² (design). St = 75% × yield, capped at 260 N/mm² (test). For carbon/carbon-manganese steel above 100°C design metal temperature, use the certified yield at that temperature instead (§9.1.2, not applied automatically here).
Result
Allowable design stress S—
Allowable test stress St—
Shell Course Minimum Thickness (§9.2.2, Eq.3–4)
Design pressure may be neglected if ≤10 mbar (§9.2.2 note). Test pressure pt = 1.1×p automatically if p>10 mbar, else 0. Corrosion allowance is added directly in the design-condition formula only.
Result
Design pressure used (0 if ≤10 mbar)—
Test pressure pt (1.1×p)—
Shell thickness, design condition ec—
Shell thickness, test condition et—
Governing thickness (greater of ec, et)—
Also check §9.1.5 (Table 16): the specified thickness shall never be less than the minimum nominal thickness banded by tank diameter and material — not computed here, cross-check separately. Maximum specified shell/reinforcing plate thickness is 40mm (§9.1.6); no course shall be thinner than the course above it, except the top compression area (§9.1.7).