Stress & Strain.

Stress & Strain.

Stress: When a material in subjected to an external force, a resisting force is set up within the component. The internal resistance force per unit area acting on a material is called the stress at a point. It is a scalar quantity having unit.

Types of Stresses:

Normal stressShear StressBulk Stress

Strain: It is the deformation produced in the material due to simple stress. It usually represents the displacement between particles in the body relative to a reference length.

F is expressed in Newton (N) and A, original area, in square meters (m2), the stress σ will be expresses in N/ m2. This unit is called Pascal (Pa).

• As Pascal is a small quantity, in practice, multiples of this unit is used.

                               

Types of Strains:

Normal Strain

Since strain is m/m it is dimensionless.

Shear strainNote 1: The angle is radians, not degrees. The volume of the solid is not changed by shear strain.

 

Note: the angle is radians, not degrees

Bulk Strain True Stress and True StrainThe true stress is defined as the ratio of the load to the cross section area at any instant.

   Where σ and ε is the engineering stress and engineering strain respectively.

The true strain is defined as

The volume of the specimen is assumed to be constant during plastic deformation.

Stress-Strain Relationship

The stress-strain diagram is shown in the figure. In brittle materials there is no appreciable change in rate of strain. There is no yield point and no necking takes place.

Graph between stress-strain

In figure (a), the specimen is loaded only upto point A, is gradually removed the curve follows the same path AO and strain completely disappears. Such a behavior is known as the elsastic behavior.

In figure (b), the specimen is loaded upto point B beyond the elastic limit E. When the specimen is gradually loaded the curve follows path BC, resulting in a residual strain OC or permanent strain.

Comparison of engineering stress and the true stress-strain curves shown below:

The true stress-strain curve is also known as the flow curve.

• True stress-strain curve gives a true indication of deformation characteristics because it is based on the instantaneous dimension of the specimen.

• In engineering stress-strain curve, stress drops down after necking since it is based on the original area.

• In true stress-strain curve, the stress however increases after necking since the cross sectional area of the specimen decreases rapidly after necking.

• The flow curve of many metals in the region of uniform plastic deformation can be expressed by the simple power law.

                                                                                 σT = K(εT)n

  Where K is the strength coefficient

   n is the strain hardening exponent

   n = 0 perfectly plastic solid

   n = 1 elastic solid For most metals, 0.1< n < 0.5

Properties of Materials

Some properties of materials which judge the strength of materials are given below:

Elasticity: Elasticity is the property by virtue of which a material is deformed under the load and is enabled to return to it original dimension when the load is removed.

Plasticity: Plasticity is the converse of elasticity. A material in plastic state is permanently deformed by the application of load and it has no tendency to recover. The characteristic of the material by which it undergoes inelastic strains beyond those at elastic limit is known as plasticity.

Ductility: Ducitility is the characteristic which permits a material to be drawn out longitudinally to a reducd section, under the action of a tensile force (large deformation).

Brittleness: Brittleness implies lack of ductility. A material is said to be brittle when it cannot be drawn out by tension to smaller section.

Malleability

Malleability is a property of a material which permits the material to be extended in all directions without rapture. A malleable material possess a high degree of plasticity, but not necessarily great strength.

Toughness

Toughness is the property of a material which enable it to absorb energy without fracture.

Hardness

Hardness is the ability of a material to resist indentation or surface abrasion. Brinell hardness test is used to check hardness.

Brinell Hardness Number (BHN)

where, P = Standard load, D = Diameter of steel ball

d = Diameter of the indent.

Strength

The strength of a material enables it to resist fracture under load.

Engineering Stress-Strain Curve

The stress-strain diagram is shown in figure. The curve start from origin. Showing thereby that there is no initial stress of strain in the specimen.

The stress-strain curve diagram for a ductile material like mild steel is shown in figure below.

* Upto point A, Hooke's Law is obeyed and stress is proportional to strain. Point A is called limit of proportionality.

* Point B is called the elastic limit point.

* At point B the cross-sectional area of the material starts decreasing and the stress decreases to a lower value to point D, called the lower yield point.

* The apparent stress decreases but the actual or true stress goes on increasing until the specimen breaks at point C, called the point of fracture.

* From point E ownward, the strain hardening phenomena becomes predominant and the strength of the material increases thereby requiring more stress for deformation, until point F is reached. Point F is called the ultimate point.

 

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Elastic Constants.

Elastic Constants.

Elastic Constants: Stress produces a strain, but how much strain is produced depends on the solid itself. The solid is then characterised by anelastic modulus that relates strain to stress.>

Different types of stresses and their corresponding strains within elastic limit are related which are referred to as elastic constants. The three types of elastic constants (moduli) are:

Modulus of elasticity or Young’s modulus (E),Bulk modulus (K) andModulus of rigidity or shear modulus (M, C or G).Young’s modulus

Rigidity modulus

Bulk modulus

 

 Poisson’s Ratio (µ): is defined as ratio of lateral strain to axial or longitudinal strain

Poisson Ratio=-(Transverse Strain/Axial Strain)

 (Under unidirectional stress in x-direction)

Young’s modulus or Modulus of elasticity (E) = (PL /Aδ)= σ/∈ Modulus of rigidity or Shear modulus of elasticity (G) =τ/γ= PL /Aδ Bulk Modulus or Volume modulus of elasticity (K) = -(Δ p/p)/(Δv/v) =(Δp)/(ΔR/R )

 

Relationship between the elastic constants E, G, K, µ :

where K = Bulk Modulus, μ= Poisson’s Ratio, E= Young’s modulus, G= Modulus of rigidity

 

Hooke's Law (Linear elasticity)

Hooke's Law stated that within elastic limit, the linear relationship between simple stress and strain for a bar is expressed by equations.

Where, E = Young's modulus of elasticity

P = Applied load across a cross-sectional area

Δl = Change in length

l = Original length

 Free expansion of 1 due to temperature rise

 Free expansion of 2 due to temperature rise

 Expansion of 1 due to temperature stress (tensile)

 Compression of 2 due to temperature stress (compression)

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Poisson's Ratio.

Poisson's Ratio.

Poisson's Ratio: The three stresses and strains do not operate independently. Stresses produce strains in lateral directions as the solid tries to retain its original volume. Poisson's ratio is a measure of how successful this is.

When an axial force is applied along the longitudinal axis of a bar, the length of a bar will increase but at the same time its lateral dimension (width) will be decreased so, it is called as Poisson' ratio.

Value of Poisson's ratio is same in tension and compression

Under uniaxial loading0≤ μ ≤ 0.5μ = 0 for corkμ = 0.5 For perfectly plastic body(Rubber)μ = 0.25 to 0.42 for elastic metalsμ = 0.1 to 0.2 for concreteμ = 0.286 mild steelμ is greater for ductile metals than for brittle metals. Volumetric Strain

It is defined as the ratio of change in volume to the initial volume. Mathematically

Volumetric strain,

 

Volumetric Strain Due to Single Direct Stress

The ratio of change in volume to original volume is called volumetric strain.

ev = e1 + e2 + e3


Volumetric strain:

For the circular bar of diameter d:

 

Volumetric Strain due to Three Mutually Perpendicular Stress System: When a body is subjected to identical pressure in three mutually perpendicular direction, then the body undergoes uniform changes in three directions without undergoing distortion of shape.

or 

 

 

Shear Modulus or Modulus of Rigidity

Modulus of rigidity :

* At principal planes, shear stress is always zero.

* Planes of maximum shear stress also contains normal stress.

 

Relationship between E, G, K and μ :

Modulus of rigidity:

 

Bulk modulus:

 

 

 

 

 

 

Analysis of Stress and Strain

We will derive some mathematical expressions for plains stresses and will study their graphical significance in 2D and 3D

 

Stress on Inclined Section PQ due to Uniaxial Stress

Consider a rectangular cross-section and we have to calculate the stress on an inclined section as shown in figure.

Normal stress :

Stress on an inclined section

Tangential stress

Resultant stress

 

Stress Induced by State Simple Shear

Induced stress is divided into two components which are given as

Normal stress: 

Tangential stress:

 

Stress Induced by Axial Stress and Simple Shear

Normal stress

 

Tangential stress

 

Principal Stresses and Principal Planes

The plane carrying the maximum normal stress is called the major principal plane and normal stress is called major principal stress. The plane carrying the minimum normal stress is known as minor principal stress.

 

Major principal stress :

Minor principal stress :

Across maximum normal stresses acting in plane shear stresses are zero.

 

Computation of Principal Stress from Principal Strain

The three stresses normal to shear principal planes are called principal stress, while a plane at which shear strain is zero is called principal strain.

For two dimensional stress system, σ3 = 0

 

Maximum Shear Stress

The maximum shear stress or maximum principal stress is equal of one half the difference between the largest and smallest principal stresses and acts on the plane that bisects the angle between the directions of the largest and smallest principal stress, i.e., the plane of the maximum shear stress is oriented 45° from the principal stress planes.

 

Principal Strain

For two dimensional strain system,

Where, e1 = Strain in x-direction

e2 = Strain in y-direction

φ = Shearing strain relative to OX and OY

Maximum Shear Strain:

The maximum shear strain also contains normal strain which is given as

45° Strain Rosette or Rectangular Strain Rosette

Rectangular strains Rosette are inclined 45° to each other

Principal strains:

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