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MAYURBHANJ SCHOOL OF ENGINEERING,BARIPADA

Branch : Automobile Engineering�Semester : 5th Sem, WINTER :2021

Subject : TH5- Automobile Component Design

Chapter : 01 Introduction

Topic : Machine Design Basic Concept and properties of material

Faculty : Er. Sidhartha Kumar Mohanta

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  • Normal Load (Axial load): Load is perpendicular to the

supporting material.

- Tension Load: As the ends of material are pulled apart

to make the material longer, the load is called a tension

load.

- Compression Load: As the ends of material are pushed in

to make the material smaller, the load is called

a compression load.

Tension

Compression

Classifying Loads on Materials

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  • Shear Load : Tangential load

pulling apart

Pressure

Cargo

Classifying Loads on Materials

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Stress and Strain

In order to compare materials, we must have measures.

  • Stress : load per unit Area

F : load applied in pounds

A : cross sectional area in in²

: stress in psi

A

F

F

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  • Strain:

- Ratio of elongation of a material to the original length

- unit deformation

e : elongation (ft)

Lo : unloaded(original) length of a material (ft)

: strain (ft/ft) or (in/in)

Elongation:

L : loaded length of a material (ft)

Lo

e

L

Stress and Strain

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Baldwin Hydraulic Machine for Tension & Compression test

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Stress-Strain Diagram

  • A plot of Strain vs. Stress.
  • The diagram gives us the behavior of the material and

material properties.

  • Each material produces a different stress-strain

diagram.

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Strain ( ) (e/Lo)

4

1

2

3

5

Stress (F/A)

Elastic

Region

Plastic

Region

Strain

Hardening

Fracture

ultimate

tensile strength

Slope=E

Elastic region

slope=Young’s(elastic) modulus

yield strength

Plastic region

ultimate tensile strength

strain hardening

fracture

necking

yield

strength

Stress-Strain Diagram

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  • Elastic Region (Point 1 –2)

- The material will return to its original shape

after the material is unloaded( like a rubber band).

- The stress is linearly proportional to the strain in

this region.

: Stress (psi)

E : Elastic modulus (Young’s Modulus) (psi)

: Strain (in/in)

  • Point 2 : Yield Strength : a point at which permanent

deformation occurs. ( If it is passed, the material will

no longer return to its original length.)

or

Stress-Strain Diagram

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Plastic Region (Point 2 –3)

- If the material is loaded beyond the yield strength,

the material will not return to its original shape

after unloading.

- It will have some permanent deformation.

- If the material is unloaded at Point 3, the curve will

proceed from Point 3 to Point 4. The slope will be

the as the slope between Point 1 and 2.

- The distance between Point 1 and 4 indicates the

amount of permanent deformation.

Stress-Strain Diagram

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Strain Hardening

- If the material is loaded again from Point 4, the

curve will follow back to Point 3 with the same

Elastic Modulus(slope).

- The material now has a higher yield strength of

Point 4.

- Raising the yield strength by permanently straining

the material is called Strain Hardening.

Stress-Strain Diagram

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Tensile Strength (Point 3)

- The largest value of stress on the diagram is called

Tensile Strength(TS) or Ultimate Tensile Strength

(UTS)

- It is the maximum stress which the material can

support without breaking.

Fracture (Point 5)

- If the material is stretched beyond Point 3, the stress

decreases as necking and non-uniform deformation

occur.

- Fracture will finally occur at Point 5.

Stress-Strain Diagram

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A36 Steel

Stress-Strain Diagram

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5.4 Material Properties

  • Strength
  • Hardness
  • Ductility
  • Brittleness
  • Toughness

Characteristics of Material are described as

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Strength:

- Measure of the material property to resist deformation

and to maintain its shape

- It is quantified in terms of yield stress or ultimate

tensile strength .

- High carbon steels and metal alloys have higher strength

than pure metals.

- Ceramic also exhibit high strength characteristics.

Material Properties

σult

σy

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Hardness:

- Measure of the material property to resist indentation,

abrasion and wear.

- It is quantified by hardness scale such as Rockwell and

Brinell hardness scale that measure indentation /

penetration under a load.

- Hardness and Strength correlate well because both

properties are related to inter-molecular bonding. A

high-strength material is typically resistant to wear

and abrasion.

Material Properties

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Ductility:

- Measure of the material property to deform before failure.

- It is quantified by reading the value of strain at the

fracture point on the stress strain curve.

- Ductile materials can be pulled or drawn into pipes, wire,

and other structural shapes

- Examples of ductile material :

low carbon steel

aluminum

copper

brass

Material Properties

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Brittleness:

- Measure of the material’s inability to deform before failure.

- The opposite of ductility.

- Example of ductile material : glass, high carbon steel,

ceramics

Ductile

Brittle

Stress

Strain

Material Properties

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Toughness:

- Measure of the material ability to absorb energy.

- It is measured by two methods.

a) Integration of stress strain curve

- Slow absorption of energy

- Absorbed energy per unit volume

unit : (lb/in²) *(in/in) =lb·in/in³

b) Charpy test

- Ability to absorb energy of an impact without

fracturing.

- Impact toughness can be measured.

Material Properties

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Charpy V-Notch Test:

Material Properties

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Fatigue:

  • The repeated application of stress typically produced by

an oscillating load such as vibration.

  • Sources of ship vibration are engine, propeller and waves.

Cycles N at Fatigue Failure

Stress (psi)

Steel

Aluminum

Endurance Limit : A certain threshold

stress which will not cause the fatigue

failure for the number of cycles.

Aluminum has no endurance limit

Material Properties

MAXIMUM stress decreases as the number of loading cycles increases.

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Example:

Mooring line length =100 ft

diameter=1.0 in

Axial loading applied=25,000 lb

Elongation due to loading=1.0 in

mooring line

loading

1) Find the normal stress.

2) Find the strain.

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Example:

- Salvage crane is lifting an object of 20,000 lb.

- Characteristics of the cable

diameter=1.0 in, length prior to lifting =50 ft

1) Find the normal stress in the cable.

2) Find the strain.

3) Determine the cable stretch in inches.

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THANK YOU