Cylinder Stress Calculator

Calculate hoop, axial, and radial stresses in thin-walled and thick-walled pressure vessels. Verify design safety factors per ASME codes.

Hoop Stress (inner)
105.2 MPa
Lamé (thick-wall)
Axial Stress
47.6 MPa
Closed-end condition
Radial Stress (inner)
-10.0 MPa
= -Pi at inner surface
von Mises Stress
99.8 MPa
At inner surface
Safety Factor (Hoop)
2.38
✓ Adequate
r/t Ratio
10.0
Thick-wall analysis needed

Stress Through Wall Thickness

r=100
105
r=102
103
r=104
101
r=106
99
r=108
97
r=110
95
Blue = hoop stress (MPa) at various radial positions

Thickness vs Stress & Safety Factor

Thickness (mm)Hoop Stress (MPa)Safety Factor
5205.11.22
8130.21.92
10105.22.38
1288.62.82
1572.03.47
2055.54.51
2545.65.49
3039.06.41
4030.88.11
5026.09.62
Stress Summary & ASME
ComponentInner SurfaceOuter Surface
Hoop (σ_h)105.2 MPa95.2 MPa
Axial (σ_a)47.6 MPa47.6 MPa
Radial (σ_r)-10.0 MPa-0.0 MPa
von Mises99.8 MPa

ASME VIII Div.1 minimum thickness (simplified): 8.4 mm (current: 10 mm, ✓ OK)

Planning notes, formulas, and examples

About the Cylinder Stress Calculator

The Cylinder Stress Calculator determines hoop (circumferential), axial (longitudinal), and radial stresses in cylindrical pressure vessels under internal and/or external pressure. The tool handles both thin-walled (r/t > 10) and thick-walled (r/t ≤ 10) cylinders using the appropriate equations.

For thin-walled vessels, the simple formulas σ_h = pr/t and σ_a = pr/(2t) apply. For thick-walled vessels, the Lamé equations account for the stress variation through the wall thickness — stress is highest on the inner surface and decreases toward the outer surface. This distinction is critical for high-pressure applications (>1000 psi) and thick-walled tubes.

Enter the vessel geometry, pressure conditions, and material yield strength to calculate all stress components, verify the safety factor, and determine minimum required wall thickness per ASME Section VIII guidelines. It gives you a fast sanity check before you move to a more detailed design review. That is useful when you want a quick pass/fail check before doing a deeper vessel analysis.

When This Page Helps

Use this calculator when you need to check hoop, axial, and radial stress in a pressurized cylinder before committing to a wall thickness. It is useful for vessel design, pipe checks, and quick ASME-style sanity checks. That is especially helpful when you want to compare a thin-wall estimate against a thick-wall case quickly.

How to Use the Inputs

  1. Enter the inner radius (or diameter) of the cylinder.
  2. Enter the wall thickness.
  3. Enter internal pressure (and external pressure if applicable).
  4. Enter the material yield strength.
  5. Review hoop, axial, and radial stresses at inner and outer surfaces.
  6. Check the safety factor against the material yield strength.
Formula used
Thin-Wall: σ_hoop = p×r/t, σ_axial = p×r/(2t). Thick-Wall (Lamé): σ_h = (p_i×r_i² - p_o×r_o²)/(r_o² - r_i²) + (p_i - p_o)×r_i²×r_o²/[r²×(r_o² - r_i²)]. σ_r = (p_i×r_i² - p_o×r_o²)/(r_o² - r_i²) - (p_i - p_o)×r_i²×r_o²/[r²×(r_o² - r_i²)]. σ_a = (p_i×r_i² - p_o×r_o²)/(r_o² - r_i²).

Example Calculation

Result: Hoop stress = 105 MPa, Safety factor = 2.38

r/t = 100/10 = 10 (borderline thin/thick). Thin-wall: σ_h = 10×100/10 = 100 MPa. Thick-wall (at inner surface): σ_h = 105 MPa. Axial: σ_a = 50 MPa. von Mises: 91.0 MPa. Safety factor = 250/105 = 2.38.

Tips & Best Practices

  • Hoop stress always governs for internal pressure — it's the highest stress component.
  • For thick vessels, maximum stress is always at the inner surface where r = r_i.
  • Corrosion allowance: add 1/8" (3mm) or more to calculated wall thickness for carbon steel.
  • Weld joint efficiency E = 1.0 requires full radiographic examination of all welds.
  • Consider proof testing new vessels at 1.3-1.5× design pressure to verify integrity.

Thin-Wall vs Thick-Wall Theory

Thin-wall theory (also called membrane theory) assumes that stress is uniform through the wall thickness. This simplification works well when the thickness is small relative to the radius (t/r < 0.1 or r/t > 10). The resulting formulas are simple: σ_hoop = pr/t, σ_axial = pr/(2t).

Thick-wall theory (Lamé equations, 1833) accounts for the variation of stress through the wall. At the inner surface, hoop stress is higher than the thin-wall prediction. At the outer surface, it's lower. The average through the thickness equals the thin-wall value. For a vessel with r_i/r_o = 0.5 (very thick wall), the inner surface hoop stress exceeds the thin-wall value by about 67%.

ASME Design Guidelines

ASME Section VIII provides rules for unfired pressure vessels. Division 1 (design-by-rule) uses the maximum normal stress theory with safety factors applied to the allowable stress. Division 2 (design-by-analysis) allows detailed stress analysis with different limits for primary membrane, primary bending, secondary, and peak stresses. Division 2 typically results in thinner walls because it uses more accurate stress classification.

von Mises Equivalent Stress

For multiaxial stress states, the von Mises criterion provides a single equivalent stress: σ_vm = √[(σ_h - σ_a)² + (σ_a - σ_r)² + (σ_r - σ_h)²] / √2. Yielding occurs when σ_vm equals the uniaxial yield strength. For internal pressure vessels, the von Mises stress is about 13% lower than the maximum principal stress (hoop stress), which provides additional design margin when using the maximum stress criterion.

Sources & Methodology

Last updated:

Frequently Asked Questions

  • Use thick-wall (Lamé) equations when r/t ≤ 10, or when the stress variation through the wall exceeds 5% (which happens when t > 0.1×r). Thin-wall formulas assume uniform stress across the thickness, which becomes inaccurate for thick walls. Always use thick-wall for high-pressure applications.