mechanics of materials ii uet, taxila lecture no. (6)

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Mechanics of Materials II UET, Taxila Lecture No. (6)

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Page 1: Mechanics of Materials II UET, Taxila Lecture No. (6)

Mechanics of Materials II

UET, TaxilaLecture No. (6)

Page 2: Mechanics of Materials II UET, Taxila Lecture No. (6)

Cylinders & Pressure vessels

Cylindrical or spherical pressure vessels are commonly used in industry to carry both liquids and gases under pressure.

Page 3: Mechanics of Materials II UET, Taxila Lecture No. (6)

Classification of applications Cylinders find many applications,

two of the most common categories being :

a- fluid containers such as : pressure vessels, hydraulic

cylinders, gun barrels, pipes, boilers and tanks.

b- interference-fitted bearing bushes, sleeves and the like.

Page 4: Mechanics of Materials II UET, Taxila Lecture No. (6)

Other applications

Cylinders can act as beams or shafts eg. ( load building blocks) but in the present chapter cylinders are loaded primarily by internal and external pressures due to adjacent fluids or to contacting cylindrical surfaces.

Page 5: Mechanics of Materials II UET, Taxila Lecture No. (6)

Pressure Loading

When the pressure vessel is exposed to this pressure, the material comprising the vessel is subjected to pressure loading, and hence stresses, from all

directions.

Page 6: Mechanics of Materials II UET, Taxila Lecture No. (6)

Factors that affect stresses

The normal stresses resulting from this pressure are function of :

1- the radius of the element under consideration,

2- the shape of the pressure vessel (i.e., open ended cylinder, closed end cylinder, or sphere)

3- the applied pressure.

Page 7: Mechanics of Materials II UET, Taxila Lecture No. (6)

Two types of analysis are commonly applied to pressure vessels.

The most common method is based on a simple mechanics approach and is applicable to “thin wall” pressure vessels which by definition have a ratio of inner radius (r), to wall thickness (t) of r/t ≥ 10.

Page 8: Mechanics of Materials II UET, Taxila Lecture No. (6)

The second method is based on elasticity solution and is always applicable

regardless of the r/t ratio and can be referred to as the solution for “thick wall” pressure vessels.

Page 9: Mechanics of Materials II UET, Taxila Lecture No. (6)

Limiting proportions (approx)    

Thin Thick d/t > 20 d/t < 20

t/d < 1/20 t/d > 1/20

t/d < 0.05 t/d > 0.05

Where d = Di = inner diameter t = Cylinder thickness

Page 10: Mechanics of Materials II UET, Taxila Lecture No. (6)

Thin-Walled Pressure Assumptions

Several assumptions are made in this method.

1) Plane sections remain plane2) r/t ≥ 10 with t being uniform and

constant3) The applied pressure, p, is the gauge

pressure (where p is the difference between the absolute pressure and the atmospheric pressure)

Page 11: Mechanics of Materials II UET, Taxila Lecture No. (6)

4) Material is linear-elastic, isotropic and homogeneous.

5) Stress distributions throughout the wall thickness will not vary

6) Element of interest is remote from the end of the cylinder and other geometric discontinuities.

7) Working fluid has negligible weight.

Page 12: Mechanics of Materials II UET, Taxila Lecture No. (6)

THIN CYLINDERS AND SHELLS

1- THIN CYLINDERS

Page 13: Mechanics of Materials II UET, Taxila Lecture No. (6)

Thin cylinder representation

Page 14: Mechanics of Materials II UET, Taxila Lecture No. (6)

Classifications of Cylinders

Cylinders are classed as being either :

open - in which there is no axial component of wall stress, or

closed - in which an axial stress must exist to equilibrate the fluid pressure.

Page 15: Mechanics of Materials II UET, Taxila Lecture No. (6)

Different types of open & closed Cylinders

Page 16: Mechanics of Materials II UET, Taxila Lecture No. (6)

When a thin-walled cylinder is subjected to internal pressure, three mutually perpendicular principal stresses will be set up in the cylinder material.

Page 17: Mechanics of Materials II UET, Taxila Lecture No. (6)

Types of stresses

Namely:1- The circumferential or hoop stress.

2- The longitudinal stress.

3- The radial stress.

Page 18: Mechanics of Materials II UET, Taxila Lecture No. (6)

Provided that the ratio of thickness to inside diameter of the cylinder is less than 1/20, it is reasonably accurate to assume that the hoop and longitudinal stresses are constant across the wall thickness.

Page 19: Mechanics of Materials II UET, Taxila Lecture No. (6)

Also, the magnitude of the radial stress set up is so small in comparison with the hoop and longitudinal stresses that it can be neglected.

Page 20: Mechanics of Materials II UET, Taxila Lecture No. (6)

This is obviously an approximation since, in practice, it will vary from zero at the outside surface to a value equal to the internal pressure at the inside surface.

Page 21: Mechanics of Materials II UET, Taxila Lecture No. (6)

For the purpose of the initial derivation of stress formulae it is also assumed that the ends of the cylinder and any riveted joints present have no effect on the stresses produced; in practice they will have an effect and this will be discussed later.

Page 22: Mechanics of Materials II UET, Taxila Lecture No. (6)

Thin cylinders under internal pressure

Page 23: Mechanics of Materials II UET, Taxila Lecture No. (6)

Hoop or circumferential stress

Page 24: Mechanics of Materials II UET, Taxila Lecture No. (6)

1- Hoop or circumferential stress

This is the stress which is set up in resisting the bursting effect of the applied pressure and can be most conveniently treated by considering the equilibrium of half of the cylinder.

Page 25: Mechanics of Materials II UET, Taxila Lecture No. (6)

It is required to calculate the hoop stress in terms of:

Pressure (p)Inner diameter (d)Thickness (t)

Page 26: Mechanics of Materials II UET, Taxila Lecture No. (6)

Half of a thin cylinder subjected to internal pressure showing the hoop and longitudinal stresses acting on any element in the cylinder surface.

Page 27: Mechanics of Materials II UET, Taxila Lecture No. (6)

Consider the equilibrium of forces in the x-direction acting on the sectioned cylinder shown in figure 2. It is assumed that the circumferential stress H (or θ( is constant through the thickness of the cylinder.

Page 28: Mechanics of Materials II UET, Taxila Lecture No. (6)

Figure (2)

Page 29: Mechanics of Materials II UET, Taxila Lecture No. (6)

Using the force equilibrium to derive an equation for hoop

stress

Page 30: Mechanics of Materials II UET, Taxila Lecture No. (6)

Calculating the total force owing to internal pressure

Total force on half-cylinder owing to internal pressure

Page 31: Mechanics of Materials II UET, Taxila Lecture No. (6)

Resisting force owing to hoop stress

Total resisting force owing to hoop

stress H set up in the cylinder walls=

Force =

Page 32: Mechanics of Materials II UET, Taxila Lecture No. (6)

Final form of hoop stress

Page 33: Mechanics of Materials II UET, Taxila Lecture No. (6)

Longitudinal stress

Page 34: Mechanics of Materials II UET, Taxila Lecture No. (6)

Longitudinal stress

Consider now the cylinder shown in Next Figure.

Cross-section of a thin cylinder.

Page 35: Mechanics of Materials II UET, Taxila Lecture No. (6)

End Section of Cylindrical Thin-Walled PressureVessel Showing Pressure and Internal Axial

Stresses

Page 36: Mechanics of Materials II UET, Taxila Lecture No. (6)

Using the force equilibrium to derive

an equation for longitudinal stress

Page 37: Mechanics of Materials II UET, Taxila Lecture No. (6)

Now consider the equilibrium of forces in the z-direction acting on the part cylinder shown in next figure .

Page 38: Mechanics of Materials II UET, Taxila Lecture No. (6)
Page 39: Mechanics of Materials II UET, Taxila Lecture No. (6)

Force owing to internal pressure

Total force on the end of the cylinder owing to internal pressure

Force on cylinder end :Force =

Page 40: Mechanics of Materials II UET, Taxila Lecture No. (6)

For equilibrium of forces we need to calculate the End

section area

Page 41: Mechanics of Materials II UET, Taxila Lecture No. (6)

End Section Area

The cross-sectional area of the cylinder wall is characterized by the product of its wall thickness and the mean circumference

For the thin-wall pressure vessels where D >> t

the cylindrical cross-section area may be

approximated by pDt.

ttD

Page 42: Mechanics of Materials II UET, Taxila Lecture No. (6)
Page 43: Mechanics of Materials II UET, Taxila Lecture No. (6)

Longitudinal stress final form

Page 44: Mechanics of Materials II UET, Taxila Lecture No. (6)

Changes in dimensions:

Page 45: Mechanics of Materials II UET, Taxila Lecture No. (6)

(a) Change in length

The change in length of the cylinder may be determined from the longitudinal strain by neglecting the radial stress.

Page 46: Mechanics of Materials II UET, Taxila Lecture No. (6)

From Hooke’s Law

Page 47: Mechanics of Materials II UET, Taxila Lecture No. (6)

And change in length = longitudinal strain x original length

Then change in length =

Page 48: Mechanics of Materials II UET, Taxila Lecture No. (6)

(b) Change in diameter

As above, the change in diameter may be determined from the strain on a diameter, i.e. the diametral strain.

Page 49: Mechanics of Materials II UET, Taxila Lecture No. (6)

Now the change in diameter may be found from a consideration of the circumferential change.

The stress acting around a circumference is the hoop or circumferential stress H

giving rise to the circumferential strain H.

Page 50: Mechanics of Materials II UET, Taxila Lecture No. (6)
Page 51: Mechanics of Materials II UET, Taxila Lecture No. (6)
Page 52: Mechanics of Materials II UET, Taxila Lecture No. (6)
Page 53: Mechanics of Materials II UET, Taxila Lecture No. (6)

Change in Diameter