This section provides a very useful introduction to the concepts of direct and shear stress and strain as encountered in mechanical engineering structures. The standard notation used is explained in some detail. Young’s modulus is introduced and explained with worked examples of standard types of simple calculations. Factors of safety are examined and their importance is explored with once again some sample calculations included. Some simple examples of basic shear stress are also given.
Objective of the experiment:
1 - Study the relationship between the force (P) and
elongation (ΔL).
2 - Stability and study the relationship between strain (ε)
and stress (σ).
3 - Study the concept of the mechanical properties of solids.
4 - Establish a modulus of elasticity (E)
Maximum principal stress theory.
Maximum shear stress theory.
Maximum shear strain theory.
Maximum strain energy theory.
Maximum shear strain energy theory.
CONTENT:
1. Elastic strain energy
2. Strain energy due to gradual loading
3. Strain energy due to sudden loading
4. Strain energy due to impact loading
5. Strain energy due to shock loading
6. Strain energy due to shear loading
7. Strain energy due to bending (flexure)
8. Strain energy due to torsion
9. Examples
When a body is subjected to gradual, sudden or impact load, the body deforms and work is done upon it. If the elastic limit is not exceed, this work is stored in the body. This work done or energy stored in the body is called strain energy.
When a body is subjected to gradual, sudden or impact load, the body deforms and work is done upon it. If the elastic limit is not exceed, this work is stored in the body. This work done or energy stored in the body is called strain energy.
This document gives the class notes of Unit 3 Compound stresses. Subject: Mechanics of materials.
Syllabus contest is as per VTU, Belagavi, India.
Notes Compiled By: Hareesha N Gowda, Assistant Professor, DSCE, Bengaluru-78.
Some basic defintions of the topics used in Strength of Materials subject. Pictorial presentation is more than details. Many examples are provided as well.
Objective of the experiment:
1 - Study the relationship between the force (P) and
elongation (ΔL).
2 - Stability and study the relationship between strain (ε)
and stress (σ).
3 - Study the concept of the mechanical properties of solids.
4 - Establish a modulus of elasticity (E)
Maximum principal stress theory.
Maximum shear stress theory.
Maximum shear strain theory.
Maximum strain energy theory.
Maximum shear strain energy theory.
CONTENT:
1. Elastic strain energy
2. Strain energy due to gradual loading
3. Strain energy due to sudden loading
4. Strain energy due to impact loading
5. Strain energy due to shock loading
6. Strain energy due to shear loading
7. Strain energy due to bending (flexure)
8. Strain energy due to torsion
9. Examples
When a body is subjected to gradual, sudden or impact load, the body deforms and work is done upon it. If the elastic limit is not exceed, this work is stored in the body. This work done or energy stored in the body is called strain energy.
When a body is subjected to gradual, sudden or impact load, the body deforms and work is done upon it. If the elastic limit is not exceed, this work is stored in the body. This work done or energy stored in the body is called strain energy.
This document gives the class notes of Unit 3 Compound stresses. Subject: Mechanics of materials.
Syllabus contest is as per VTU, Belagavi, India.
Notes Compiled By: Hareesha N Gowda, Assistant Professor, DSCE, Bengaluru-78.
Some basic defintions of the topics used in Strength of Materials subject. Pictorial presentation is more than details. Many examples are provided as well.
The aim of this unit is to investigate a number of major scientific principles that underpin the design and operation of engineering systems. It is a broad-based unit, covering both mechanical and electrical principles. It is intended to give an overview that will provide the basis for further study in specialist areas of engineering.
This unit covers Types of stresses & strains,
Hooke’s law, stress-strain diagram,
Working stress,
Factor of safety,
Lateral strain,
Poisson’s ratio, volumetric strain,
Elastic moduli,
Deformation of simple and compound bars under axial load,
Analysis of composite bar with varying cross section.
This section examines a method of analysing the bending moment and shear force distribution along a uniformly loaded, simply supported beam. The method used is Macaulay’s and the stages involved in this method are described in detail. The method also determines the position of the maximum bending moment, the slope and deflection at this point.
Poisson’s ratio is the ratio between lateral and axial strain in a directly loaded system. The derivation of standard equations and their further development is shown.
The use of jigs and fixtures within manufacturing is widely employed. Their design and the parameters to be taken in to account are discussed with the aid of a case study.
A graphical method to determine the shear force and bending moment distribution along a simply supported beam is given. A suitable example is used to illustrate the major steps in the process.
A sample calculation for the determination of the maximum stress values is also given.
Selecting the correct column in order to support a given load without over engineering the situation takes in many factors. This section takes a step by step approach to one method of selection. The key terminology and calculations are explored by use of a simple example. Extracts of column tables are used to extract key variables. The tables used are extracted from standard construction engineering data sheets.
Torsion or twisting is a common concept in mechanical engineering systems. This section looks at the basic theory associated with torsion and examines some typical examples by calculating the main parameters. Further examples include determination of the torque and power requirements of torsional systems.
The basic concepts associated with some elements of dynamic engineering systems and calculations are discussed. The theory associated with Linear and angular motion, energy and simple harmonic motion are outlined with sample calculations for each topic being given.
The use of flywheels to capture and store rotational kinetic energy has been used in a range of systems for the past two hundred years or so. This document explores some of the modern applications of these devices and their implications for future use. An example of the calculation of the rotational kinetic energy is given and the parameters associated with this calculation are discussed.
The requirement to provide balance for rotating systems is a vital component in ensuring long, reliable service. This document describes a graphical method that can be used to determine the out of balance forces of such a system and the correct size and position of the balance weight required to do this. A worked example of the method is shown.
Geometric tolerancing is a method which is widely used in industry when the more basic systems of tolerancing component features does not provide the required accuracy.
The system of geometric tolerancing id detailed together with the particular features of the system.
Industrial robots play an increasing role in modern production and assembly facilities. The different types of robot available and their configuration are discussed. Examples of typical uses in sectors of the engineering industry are also identified.
A major cost factor in the production of and component or assembly is its assembly. This section looks at some commonly used techniques which a designer can employ to ensure that assembly is cost effective and efficient. This is then linked to the use of jigs and fixtures for this purpose.
Within Engineering much of the real work is done in teams. Teamwork plays a vital role in successfully developing products for the market place. This file discusses the types of roles the team members can fulfil and how to get the most out of both the individual and the team as a whole.
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2. Introduction to stress and strain
Direct loading – stress and strain
Stress
When a material has a force exerted on it the material is said to be ‘stressed’.
If a rod is stretched the force is TENSILE
If a rod is squashed the force is ‘COMPRESSIVE’
Force (N)
Stress = Force / Area
=F/A
Units N/m2 or Pascal (Pa)
We give stress the letter σ (sigma)
So that σ = F/A
Extension due to load
Strain
If a material has a stress exerted on it the material will either lengthen or shorten. This is known
as STRAIN
Strain is the ratio of the extension due to the stress divided by its original length;
Strain = extension / original length
= x / l (we give strain the letter ε (Epsilon)
So ε = x/l
Example 1
A tie bar has a cross sectional area of 125mm2 and is subjected to a tensile load of 10kN.
Determine the stress.
F = 10kN and area = 125mm2
σ = F/A
= 10000/ 125 = 80 N/mm2
But 1m2 = 1000 000 mm2
so 80N/mm2 = 80MN/m2 OR MPa
(M = mega 106)
Example 2
Page 2 of 7
3. Introduction to stress and strain
A piece of steel 12 mm in diameter is compressed by a load of 15 kN. Determine the induced
stress in MPa.
F = 15kN and area = π r2 = π x 6 mm2
σ = F/A = 15000 / 113.1
= 132.63 N/mm2 or MPA
Strain example 1
A tie bar of original length 30mm is extended by 0.01mm when a tensile load is applied.
Determine the strain.
Original length = 30mm, Extension = 0.01mm
Strain, ε = x/l
= 0.01 / 30 = 3.3333 x 10-4
Note the units – There are none – it is a ratio !
Strain example 2
A steel column of 1.5 m length is compressed by 0.04mm when a compressive load is applied.
Calculate the strain in the column.
Original length = 1.5 m , Extension = 0.04mm
Strain, ε = x/l
= 0.04 / 1500 = 2.667 x 10-5
On strain calculations note that we need to be consistent with the units m/m OR
mm/mm
Modulus of Elasticity OR Young’s Modulus
Engineering materials possess a property known as ELASICITY. If a piece of material is
strained and the forces producing the strain are removed the material will regain its original
dimensions. IT IS ELASTIC.
This situation only happens up to a certain point in Engineering materials. This point is known
as;
The ELASTIC LIMIT
or LIMIT of PROPORTIONALITY
We can now link together stress and strain by using the Modulus of Elasticity or E;
Page 3 of 7
4. Introduction to stress and strain
E = Stress / Strain
= σ /ε (In the elastic range only)
The units of E are the same as stress (Pa).
But it is usually a very large number, typically GPa (Giga – 109)
Table 1 – Typical values of E for Engineering Materials
Material Approx value of E (GPa)
Rubber 0.007
Steel 210
Diamond 1200
Wood 14
Aluminium 72
Typical Plastic 1.4
Combined Example
A steel test specimen, 5 mm in diameter and 25mm long has a tensile load of 4.5kN exerted on
it. It is observed to stretch by 0.05mm under this load and revert back to its original length when
unstrained.. determine the value of E for this material.
In this example;
F = 4.5kN, Original l = 25mm, Diameter = 5 mm and Extension = 0.005mm.
Theory;
σ = F/A : ε = x/l : E = σ /ε
σ = F/A = F / π r2 = 4500 / (π x 2.52)
= 229.18 N/mm2 (MPa)
ε = x/l = 0.05 / 25
= 2 x 10 -3
And;
E = σ /ε = 229.18 x 106 / 2 x 10 -3
= 114.6 x 109 N/m2 (GPa)
Further Example
A steel specimen 6mm in diameter and originally 30mm long has a 8kN load applied to it. Under
this load it is observed to extend by 0.025mm. determine E for this material.
Page 4 of 7
5. Introduction to stress and strain
Factors of Safety
When designing a component or structure that will be under some form of stress a Factor of
Safety has to be considered to make certain that the working stresses keep within safe limits.
For a brittle material the factor of safety (FOS) is defined in terms of the Ultimate tensile
strength;
Factor of Safety = Ultimate tensile strength
Maximum working stress
For ductile materials the factor of safety is more usually defined in terms of the YIELD stress.
Yield stress is the value of the stress when the material goes from elastic to plastic.
Factor of Safety = Yield stress
Maximum working stress
Determining the factor of safety
The size of the factor of safety chosen depends on a range of conditions relating to the function
f the component or structure when in service some of them are listed below;
• Possible overloads
• Defects of workmanship
• Possible defects in material
• Deterioration due to wear, corrosion etc.
• The amount of damage that might occur if there is failure
• The possibility of the loads being applied suddenly or repeatedly
•
Worked examples
1. A cable used on a crane is made from a material with an ultimate tensile stress of 600
MPa. Determine the maximum safe working stress if a factor of safety of 4 is used.
Maximum working stress = Ultimate tensile strength
Factor of Safety
= 600 / 4 = 150 MPa
2. What is the factor of safety of a column made of a material with a UTS of 500 MPa if the
maximum working stress should be 200 MPa
Factors of Safety = UTS
Max working stress
= 500/200 = 2.5
Page 5 of 7
6. Introduction to stress and strain
Factors of Safety in SHEAR mode
Factors of safety can be used in shear mode but instead of using the UTS the material USS
(Ultimate Shear Stress) is used;
Factor of Safety = USS
Max working shear stress
Example
Determine the factor of safety used for a shear pin if the USS for the material is 300 MPa and
the maximum working stress should not exceed 100 MPa.
Factor of Safety = USS
Max working shear stress
= 300 / 100 = 3
Page 6 of 7