Handout 3 Materials Corrosion 0

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    CHE 3166: HANDOUT 3Stresses, Deformation and Fracture

    LEARNING OBJECTIVES: Part I

    Stress and Strain

    Elastic Deformation

    Plastic Deformation

    Ductility

    Toughness

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    Stress and Stress Types

    Stress (): Force (F) / Cross-sectional Area (A)

    = F / A

    a es ypes o ress Tension

    Compression Shear / Torsion

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    Common States of Stress: Ski Lift

    Simple tension: Cable

    Ao= cross sectionalarea (when unloaded)

    FF

    =F

    oA

    Torsion (shear): Drive Shaft

    M

    M Ao

    2R

    FsAc

    o

    =Fs

    A

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    Common states of stress

    Compression

    Ao

    Canyon Bridge, Los Alamos, NM

    o

    =F

    ABalanced Rock, ArchesNational Park

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    Engineering Stress and Strain

    0=Ft

    Aooriginal area

    before loading

    Area, A

    FtUnits of Stress:

    N/m2 or lb/in2

    Engineering stress,,,, 0000::::

    Ft

    =

    Lo = (L-L0)

    Engineering strain, : /2

    L/2

    Lowo

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    True Stress and Strain

    True stress, T:

    Load Fdivided by theinstantaneous cross-sectional

    area Ai (after deformation) iT

    A

    F=

    True strain,,,, ::::

    0

    ln

    l

    li

    T=

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    Elastic Deformation

    1. Initial 2. Small load 3. Unload

    bonds

    stretch

    return toInitial

    F

    F

    Linear-

    elastic

    Non-Linear-

    elastic

    Elastic Deformationis reversible

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    Plastic Deformation

    1. Initial 2. Small load 3. Unload

    planes

    stillsheared

    bondsstretch

    & planesshear

    Plastic Deformationis NOT reversible

    F

    elastic + plastic plastic

    F

    linearelastic

    linearelastic

    plastic

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    Linear Elastic Behaviour

    When stress () is proportional to strain ()

    E

    F

    -

    elastic Fsimpletensiontest

    Hooke's Law: = E

    E: Slope, a Constant, also known as: Modulus of Elasticity or Youngs Modulus Stiffness of the materials

    Materials resistance to elastic deformation

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    Youngs Modulus (E) of Different Material Types

    Magnesium,

    Aluminum

    Platinum

    Silver, Gold

    Tantalum

    Zinc, Ti

    Steel, NiMolybdenum

    Si crystal

    Glass -soda

    Si nitride

    Al oxide

    Glass fibers only

    Carbon fibers only

    Aramid fibers only

    6080

    10 0

    200

    600800

    10 001200

    400

    Cu alloys

    Tungsten

    Si carbide

    Diamond

    *

    A FRE(|| fibers)*

    CFRE(|| fibers)*

    MetalsAlloys Ceramics Polymers

    Composites/fibers

    E(GPa,

    109 Pa)

    YoungsModulus (E):

    Metals:40 400 GPa

    Polymers:

    0.2

    8

    0.6

    1

    G raphite

    Concrete

    PC

    Wood( grain)

    AFRE( fibers) *

    CFRE *

    GFRE*

    Epoxy only

    0.4

    0.8

    2

    4

    6

    10

    20

    PTF E

    HDP E

    LDPE

    PP

    Polyester

    PS

    PET

    CFRE( fibers) *

    G FRE( fibers)*

    0.2 4GPaCeramics:

    80 1200 GPa

    1GPa = 103MPa = 109N/m2

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    Effect of Temperature on Youngs Modulus (E)

    E decreases with increase in temperature

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    Yield Strength of Different Material Types

    CeramicsMetals/Alloys Composites/fibrePolymers

    y(MPa

    )

    ,

    rsbeforeyield.

    300

    400

    500600700

    1000

    2000

    a

    Steel (1020) cdSteel (4140) a

    Steel (4140) qt

    Ti (5Al-2.5Sn)a

    W (pure)

    Mo (pure)Cu (71500) cw

    ,

    mposites,since

    beforeyield.

    Room Temp. Data

    Based on data in

    Yields

    trength,

    PVC

    Hardtomeasu

    re

    sinceintension

    ,fractureusuallyoc

    cu

    Nylon 6,6

    LDPE

    70

    20

    40

    60

    50

    100

    10

    30

    200

    Tin (pure)

    Al (6061) a

    Cu (71500) hrTa (pure)Ti (pure) aSteel (1020)

    hr

    Hardtomeas

    ur

    inceramicmatrixandepoxymatrixc

    intension,

    fractureusuallyocc

    urs

    HDPEPP

    humid

    dry

    PC

    PET

    Table B4,Callister 7e.a = annealedhr = hot rolledag = aged

    cd = cold drawncw = cold workedqt = quenched &tempered

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    Tensile Strength (TS) or

    Ultimate Tensile Strength (UTS)

    yF= fracture or

    ultimate

    stren thrin

    TS

    s

    TS / UTS: Maximum stress on an engineering stress-strain curve

    strain

    Typical response of a metal Neck actsas stressconcentrator

    Engine

    stre

    Engineering strainAdapted from Fig. 6.11,

    Callister 7e.

    Metals: when noticeable necking starts.

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    Tensile Strength of Different Material Types

    Room Temp. Data

    Ceramics/Metals/Alloys

    Composites/fibres

    Polymers

    (MP

    a)

    300

    1000

    Al (6061) ag

    Cu (71500) hr

    Ti (pure) a

    Steel (1020)

    Steel (4140) a

    Steel (4140) qt

    Ti (5Al-2.5Sn) aW (pure)

    Cu (71500) cw

    2000

    3000

    5000

    Al oxide

    Diamond

    Si nitride

    GFRE(|| fiber)CFRE(|| fiber)

    AFRE(|| fiber)

    E-glass fib

    C fibersAramid fib

    a = annealedhr = hot rolledag = aged

    Si crystal

    Tensile

    strength,

    PVC

    Nylon 6,6

    10

    100 Al(6061) a

    LDPE

    PP

    PC PET

    20

    3040

    Graphite

    Concrete

    Glass-soda

    HDPE

    wood ( fiber)

    wood(|| fiber)

    1

    GFRE( fiber)CFRE( fiber)AFRE( fiber)

    cd = cold drawncw = cold workedqt = quenched & tempered

    COMPOSITES:

    AFRE = aramid-fiber reinforcedGFRE = glass-fiber reinforcedCFRE = carbon-fiber reinforced(each with 60 vol% fibers).

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    Ductility

    Plastic tensile strain at failure x 100L

    LLEL%

    o

    of

    =

    AoL

    Engineeringtensilestress,

    smaller %EL

    larger %ELf

    Engineering tensile strain,

    Another ductility measure: 100xA

    AARA%

    o

    fo-

    =

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    Engineeringtensilestress,

    Low toughness: ceramics

    High toughness: metals

    Toughness / Fracture Toughness

    Energy to break a unit volume of material

    Approximated by the area under the stress-strain curve

    Brittle fracture: elastic energyDuctile fracture: elastic + plastic energy

    Very low toughness:unreinforced polymers

    Engineering tensile strain,

    Why are metals/alloysand reinforced plastic

    so popular as structuralmaterials?

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    Mechanical Properties and Testing

    LEARNING OBJECTIVES: Part II

    Materials response to: Excessive Loading: Tensile Test

    oca ze oa ng: ar ness es Sudden Intense Loading: Impact Test

    Loading at High Temperatures: Creep Test

    Cyclic Loading: Fatigue Test

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    Excessive loading: Tensile Test

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    Tensile Test

    Tests are performed as per the ASTM, BS, DINor Australian Standards.

    A tensile test measures the resistance of amaterial to a static or slowly applied force.

    A machined specimen is placed in the testing

    machine and load is applied. A strain gage or extensometer is used to

    measure elongation.

    The stress obtained at the highest applied forceis the Tensile Strength.

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    Test providesdata:strength,stiffness,ductility

    Tensile Test

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    Other Tensile Test Data

    Yield Strength: The stress at which a

    prescribed amount of plastic deformation(commonly, 0.2%) is produced.

    specimen stretches before fracture.

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    Cup and Cone Fracture

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    Fracture: Different Types of Material

    Cup and cone fracture

    Brittle fracture

    a) Highly ductileb) Moderately ductile

    c) Brittle

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    Tensile Properties: Effect of Temperature