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009084
2026-04-10

VE0084 | Thin-Walled Spherical Vessel

Description

A thin-walled spherical vessel is loaded by inner pressure p. While neglecting self-weight, the goal is to determine the von Mises stress σMises and the radial deflection uR of the vessel.

Material Isotropic Linear Elastic Modulus of Elasticity E 210000.0 MPa
Poisson's Ratio ν 0.296 -
Geometry Spherical Shell Radius R 0.500 m
Shell Thickness t 5.000 mm
Load Pressure Internal Pressure p 5.000 MPa

Analytical Solution

The analytical solution is based on the theory of thin-walled vessels. This theory assumes the membrane stress state of the shell; thus, the following conditions have to be met:

  • The thickness of the shell can not change discontinuously.
  • The distributed loading can not change discontinuously.
  • The curvature radii and positions of centers cannot change discontinuously.
  • The outer forces including the reaction forces have to be tangential to the shell surface.

The stress state is described by the Laplace equation:

Where σ1, σ2 are stresses in meridian and parallel direction respectively and R1, R1 are the radii in the appropriate directions. For the spherical vessel, this can be simplified due to symmetry (σ1 = σ2 = σ, R1 = R2 = R) into the form:

The von Mises stress σMises can be determined from the principal stresses:

The radial deflection uR of the vessel follows from Hooke's law:

RFEM Settings

  • Modeled in RFEM 5.39 and RFEM 6.13
  • Element size lFE = 0.010 m
  • Isotropic linear elastic material is used
  • Full and eighth computational models are used

Results

Computational Model Theory
σMises [MPa]
RFEM 6
σMises [MPa]
Ratio
[-]
RFEM 5
σMises [MPa]
Ratio
[-]
Full Model 250.000 249.984 1.000 249.987 1.000
Eighth Model 249.984 1.000 249.984 1.000

 
The von Mises stress is probed from the test point A for both computational models. There are minor stress deviations on the surface due to the mesh topology.

Computational Model Theory
uR [mm]
RFEM 6
uR [mm]
Ratio
[-]
RFEM 5
uR [mm]
Ratio
[-]
Full Model 0.419 0.419 1.000 0.419 1.000
Eighth Model 0.419 1.000 0.419 1.000


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