- If the thickness of the cylinder is less than of the diameter of the cylinder, it is treated as the thin cylinder.
- It is assumed that the stresses are uniformly distributed through out the thickness of the wall.
- ‘Hoop stress’ or ‘Circumferential stress’ is given by
- ‘Longitudinal stress’ is given by
- The Maximum shear stress is given by
- Longitudinal strain is given by
- Volumetric strain is given by
Where p = internal pressure
d = diameter of cylinder
t = thickness of the cylinder
µ = Poisson's ratio
- If ‘σa’ be the permissible tensile stress for the shell material, then from strength point of view, the major principal stress ( σ ) should be less than or equal to σa Hence
THIN SPHERICAL SHELLS
- In case of thin spherical shells, longitudinal stress and circumferential stress are equal and are given by
(tensile in nature)
- The maximum shear stress,
- The strain in any direction is given by
- The volumetric strain is given by
CYLINDERS WITH HEMISPHERICAL ENDS
Let tc = thickness of the cylinder ts = thickness of the hemisphere
- Hoop stress in cylindrical part
- Hoop stress in hemispherical part
- Longitudinal stress in cylindrical part
- Longitudinal stress in hemispherical part
- Circumferential strain in hemispherical part
- Circumferential strain in cylindrical part
- For the condition of no distortion of the junction
- This means thickness of cylindrical part should be more than the hemispherical part.
- For the condition of same maximum stress in cylindrical and hemispherical parts,
THICK CYLINDRICAL SHELL
If the thickness of shell is greater than of its diameter then it is called thick shell.
In thick cylinders the circumferential stress no longer remains constant, but varies along the thickness and the radial pressure (px) is also not negligible.
The following three types of stresses are existing in thick cylinders :
(i) The radial pressure ‘px’ (compressive)
(ii) The hoop stress fx (tensile)
(iii) The longitudinal tensile stress po (tensile)
- The longitudinal stress may be given by
- Radial pressure is given by
Equation (ii) and (iii) are called Lame’s equation.
ro = outer radius of shell
ri = inner radius of shell A and B are Lame’s constant
1. Longitudinal tension is uniform across the thickness.
2. Hoop tension vary form maximum at inner face to minimum at outer face Hyperbolically.
3. Radial compression varies from maximum at inner face to zero at outer face. Hyperbolically.