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Thin Axisymmetric Shells Under Internal Pressure

When transporting and storing fluid media, organizing a technological process, using hydraulic drive and heat exchange systems, and in many other cases, it becomes necessary to operate technical objects under the influence of hydrostatic pressure.

From the point of view of strength and stiffness calculations, many of these structures may be classified as thin-walled axisymmetric shells of revolution. Mainly, these are various types of pressure vessels. Shells of this type are calculated according to the momentless theory, and only tensile stresses σm in the meridional (along the generatrix) and σt in circumferential (perpendicular to the meridional) directions are considered.

In this calculation, a thin-walled axisymmetric shell of arbitrary geometry with an internal axial radius r and a meridional radius R determined at the calculated point, and thickness t is considered. The shell is under hydrostatic pressure P. As a result of calculations, the equivalent stresses σ are found at any given point of the shell. In case of curved shell, in addition to the axial and meridional radiuses, this calculated point is characterized by a distance H to the center of the shell curvature in the meridional direction (along the shell axis).

In case of straight generatrix, the calculated point is characterized by the inner radius r and slope of the shell generatrix α (look at figure).

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INITIAL DATA

P - Internal pressure;


r - Inner radius of the shell in calculated point;


R - Meridional radius of the shell in calculated point;


Н - Distance along axis of the shell from center of circle of radius R to calculated point. It can take values from 0 to R;


t - Wall thickness;


α - Angle of inclination of the shell generatrix (Applies only with straight generatrix. In this case the parameters R and H are ignored).

RESULTS DATA

σ - Equivalent stress in calculated point.

Internal pressure (P)

Inner radius (r)

Meridional radius (R)

Distance (Н)

Wall thickness (t)

Angle of inclination (α)

Equivalent stress (σ)

Meridional stress (σm)

Circumferential stress (σt)

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BASIC FORMULAS

Meridional stress:

σm = P*r / (2t*cosα),

Circumferential stress:

(σt*cosα / r) + (σm / R) = 1 - Laplace equation.

Equivalent stress:

σ - Largest of stresses σm and σt.

INITIAL DATA

P - Internal pressure;


r - Inner radius of the shell in calculated point;


R - Meridional radius of the shell in calculated point;


Н - Distance along axis of the shell from center of circle of radius R to calculated point. It can take values from 0 to R;


t - Wall thickness;


α - Angle of inclination of the shell generatrix (Applies only with straight generatrix. In this case the parameters R and H are ignored).

RESULTS DATA

σ - Equivalent stress in calculated point.

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