Download - Strength of materials by A.Vinoth Jebaraj
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Prepared by Dr.A.Vinoth Jebaraj
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Solid Mechanics
Mechanics of Rigid Bodies Mechanics of
Deformable Bodies
Studying the external effects offorces on machine components andstructures
Studying the internal effects offorces on machine components andstructures
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Types of Loading
Tensile loading
Compressive loading
Shear loading(In plane stress)
Bending load(out of plane stress)
Torsional shear
Transverse shear
Normal loading : Tensile, compressive (out of plane)Shear loading: tangential loading or parallel loading (in planeloading)
Axial or normal load
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Direct shear
Torsional shear
Bending stresses ( out of plane stresses)
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Direct Shear
Torsion
An effect that produces shifting of horizontal planes of a material
The twisting and distortion of a material’s fibers in
response to an applied load
Torsional shear
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Direct Shear Stress - Examples
Single shear
Double shear
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Uniaxial loading Biaxial loading Triaxial loading
Different types of Loadings
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Types of strain (plane strain ,volumetric strain)Longitudinal (or) linear strainTransverse (or) lateral strain
Types of stresses ( plane stress,volumetric stress)Normal stressesShear stresses (or) tangential (or)
parallel stresses [τ] Internal resistance
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Within the elastic limit, lateral strain is directly proportional to longitudinalstrain.
This constant is known as Poisson’s ratio which is denoted by μ (or) 1/m.Note: Linear strain = - μ × Lateral strain
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Elastic Region Yielding Plastic Region
Fracture
Behavior of material during
loading
Different Stages in Loading
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Ductile materials Brittle materials
Stress Strain Curve
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Hooke’s Law
In 1678, Robert Hooke’s found that for many structural materials,within certain limits, elongation of a bar is directly proportional tothe tensile force acting on it. (Experimental finding)
Statement : Within the elastic limit, stress is directlyproportional to strain.
Where E = Young’s Modulus or Modulus of Elasticity (MPa)
Its for tensile, compressive and shear stresses
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Modulus of Rigidity [or] Shear Modulus
Statement : Within the elastic limit, shear stress is directlyproportional to shear strain.
Where G = Shear Modulus or Modulus of Rigidity (MPa)
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Bulk Modulus
When a body is subjected to three mutually perpendicular stresses,of equal intensity, then the ratio of the direct stress to thecorresponding volumetric strain is known as bulk modulus.
Total stress [σ] = σ x + σy + σ z
Total strain [ε] = ε x + εy + ε z
σ xσ x
σ y
σ y
σ z
σ z
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Analysis of Stresses in varying cross section bar
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Stress in an Inclined Plane
The plane perpendicular to the line of action of the load is a principal plane.[Because, It is having the maximum stress value and shear stress in this plane
is zero.] The plane which is at an angle of 90° will have no normal and tangential
stress.
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Max. shear stress = ½ Normal stress
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Note to Remember:
When a component is subjected to a tensile loading, thenboth tensile and shear stresses will be induced. Similarly,when it is subjected to a compressive loading, then bothcompressive and shear stresses induced.
At one particular plane the normal stress (either tensile orcompressive) will be maximum and the shear stress in thatplane will be zero. That plane is known as principal plane.That particular magnitude of normal stress is known asprincipal stress.
The magnitude of maximum principal stress will be higherwhen compare with the loads acting.
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Elastic Constants ( E, G, K and μ)
Where E = Young’s ModulusK = Bulk ModulusG [or] C = Shear Modulusμ = Poisson’s Ratio
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Principal Stresses
When a combination of axial, bending and shear loadingacts in a machine member , then identifying the plane ofmaximum normal stress is difficult . Such a plane is known asprincipal plane and the stresses induced in a principal plane isknown as principal stresses. Principal stress is an equivalentof all stresses acting in a member.
Combined loading
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Max principal normal stresses
Max principal shear stresses
Biaxial and shear loading
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Mohr’s Circle Diagram
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Thermal Stresses
When a body is subjected to heating or cooling, it will try toexpand or contract. If this expansion or contraction is restrictedby some external FORCES, then thermal stresses will beinduced.
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Actual Thermal Stresses
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Strength ability to resist external forces
Stiffness ability to resist deformation under stress
Elasticity property to regain its original shape
Plasticity property which retains the deformation producedunder load after removing load
Ductility property of a material to be drawn into wire formwith using tensile force
Brittleness property of breaking a material without anydeformation
Mechanical properties of materials
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Malleability property of a material to be rolled orhammered into thin sheets
Toughness property to resist fracture under impact load
Machinability property of a material to be cut
Resilience property of a material to absorb energy
Creep material undergoes slow and permanentdeformation when subjected to constant stress with hightemperature
Fatigue failure of material due to cyclic loading
Hardness resistant to indentation, scratch
Mechanical Properties of MaterialsContd. . .
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Bending Moment
“Bending moment = Force × Perpendicular distance between the line of the action of the force and the point
about which the moment produced”
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“Vertical force in a section which is in transverse direction perpendicular to the axis of a beam is known as transverse shear
force”
Cantilever Beam
Transverse Shear Force
Applied Load
Reaction Force
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Shear Force (S.F)
Applied force
Reaction force
Shear force
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For drawing shear force diagram, consider left or right portion of thesection in a beam.
Add the forces (including reaction) normal to the beam on one of theportion. If the right portion is chosen, a force on the right portion actingdownwards is positive while a force acting upwards is negative and viceversa for left portion.
Positive value of shear force are plotted above the base line.
S.F. Diagram will increase or decrease suddenly by a vertical straight lineat a section where there is point vertical load.
Shear force between two vertical loads will be constant.
Points to remember
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“The resultant force acting on any one portion (left or right) normal to the axis of the beam is called shear force at the section X-X. This shear force is known as
transverse shear force”
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Simply Supported Beam carrying 1000 N at its midpoint. The reactions at the supports will be equal to RA = RB = 500 N
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Pure Bending
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Assumptions in the Evaluation of Bending stress
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R = Radius of shaft, L = Length of the shaft T = Torque applied at the free endC = Modulus of Rigidity of a shaft materialτ = torsional shear stress induced at the cross sectionØ = shear strain, θ = Angle of twist
Torsional Equation
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Design for Bending
Design for Bending & Twisting
When a shaft is subjected to pure rotation, then it has to be designed for
bending stress which is induced due to bending moment caused by self
weight of the shaft.
Example: Rotating shaft between two bearings.
When a gear or pulley is mounted on a shaft by means of a key, then it
has to be designed for bending stress (induced due to bending moment)
and also torsional shear stress which is caused due to torque induced
by the resistance offered by the key .
Example: gearbox shaft (splines)
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Shear stress distribution in solid & hollow shafts
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Hoop stress (or) Circumferential stress
Circumferential or hoop Stress (σ H) = (p .d)/ 2t
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Longitudinal stress = (σ L) = (p .d)/ 4t
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Euler’s Formula for Buckling
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Both ends pinned Both ends fixed
One end fixed, other free One end fixed and other pinned