| Pressure Vessels
An EngineersToolbox Calculation Module |
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| Background Information | |||||
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This module calculates the wall stresses and deflections in homogeneous, linear elastic, isotropic, cylinders and spheres subjected to internal and/or external pressure. Stress and deflection results found by this module are valid only for wall sections remote from any stress concentration effects. Stresses and deflections in the vicinity of end caps or vessel openings must be calculated by other methods (see Reference 3). |
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| Input | |||||
| The Pressure Vessels module input
form is shown in Figure 1. Input parameters include
geometry, material properties, applied loads, and problem
description (sphere or cylinder). Material properties
may be imported from the ETB Material
Properties Database.
Figure 1. Module input form |
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| Results | |||||
The Pressure Vessels module
calculates the following:
Plotted Output Radial and hoop (circumferential) stresses can be plotted versus radial station using the standard ETB plot package shown in Figure 2.
Figure 2. Module plot results.
Text Output Input parameters and all calculated results are tabulated in the standard ETB text output window shown in Figure 3.
Figure 3. Module tabulated results. |
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| Thick-Walled Cylinder Equations | |||||
| The Pressure Vessels module
calculates the stresses and deflections of a thick-walled
cylinder subject to internal and external pressure
loading.
Figure 4. Thick-walled cylinder
Normal Stresses The geometry and stress definitions for the thick-walled cylinder problem are shown in Figure 4. The stresses in the cylinder wall are functions of the inner radius, ri, the outer radius, ro, the inner pressure, Pi, the outer pressure, Po, and a radial coordinate, r, where ri <= r <= ro. If the cylinder ends are closed and the resulting axial loads are carried by the cylinder (not by the cylinder support structure) the normal stress in the longitudinal direction, or axial stress, is given by:
If the cylinder ends are free, the axial stress is zero.
The normal stress in the circumferential direction, or hoop stress, at a radial distance r, where ri <= r <= ro, is given by:
The normal stress in the radial direction, or radial stress, at a radial distance r, where ri <= r <= ro, is given by:
Radial Deflections Radial deflections are derived from the calculated stresses using basic geometry and Hooke's law. Given a linear isotropic material with an Elastic Modulus, E, and a Poisson's Ratio, n, the radial deflection can be calculated from:
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| Thick-Walled Sphere Equations | |||||
| The Pressure Vessels module
calculates the stresses and deflections of a thick-walled
sphere subject to internal and external pressure loading.
Figure 5. Thick-walled sphere
Normal Stresses The geometry and stress definitions for the thick-walled sphere problem are shown in Figure 5. The stresses in the sphere wall are functions of the inner radius, ri, the outer radius, ro, the inner pressure, Pi, the outer pressure, Po, and a radial coordinate, r, where ri <= r <= ro.
The normal stresses in the circumferential directions are given by:
The normal stresses in the radial direction is given by:
Radial Deflection: Radial deflections are derived from the calculated stresses using basic geometry and Hooke's law. Given a linear isotropic material with an Elastic Modulus, E, and a Poisson's Ratio, n, the radial deflection can be calculated from:
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| References | |||||
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