MSE 3300-Lecture Note 09-Chapter 06 Mechanical Properties of Metals 1

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  • 8/18/2019 MSE 3300-Lecture Note 09-Chapter 06 Mechanical Properties of Metals 1

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -

    Lecture 9. Mechanical Properties

    of Metals (1)Learning Objectives

     After this lecture, you should be able to do the following:

    1. Define engineering stress and strain.

    2. Given an engineering stress–strain diagram, determine (a) the

    modulus of elasticity, (b) the yield stress, and (c) the tensile strength and

    (d) estimate the percentage elongation.

    Reading

    • Chapter 6: Mechanical Properties of Metals (6.1–6.5)

    Multimedia• Tensile tests: https://www.youtube.com/watch?v=ZwTF_-JZgt8;

    https://www.youtube.com/watch?v=67fSwIjYJ-E;

    https://www.youtube.com/watch?v=K28WiL21Sgs

    • Virtual Materials Science & Engineering (VMSE):

    http://www.wiley.com/college/callister/CL_EWSTU01031_S/vmse/

    1

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -

    1. Concepts of Stress and Strain

    2

    Stress–Strain Diagram

    Modulus of elasticity, the yield stress, and

    the tensile strength

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -

    Type of Loading

    3

    Schematic of how a load produces a deformation (strain): (a) tension, (b)

    compression, (c) shear, and (d) torsion

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 - 4

    Tension Tests: Stress-Strain Testing

    Fig. 6.3, Callister & Rethwisch 9e.

    (Taken from H.W. Hayden, W.G. Moffatt, and J. Wulff, The Structure and Properties of

    Materials, Vol. III, Mechanical Behavior , p. 2, John Wiley and Sons, New York, 1965.)

    specimen extensometer  

    • Typical tensile

    specimen

    Fig. 6.2,

    Callister &

    Rethwisch 9e. 

    gauge

    length

    • Typical tensile test

    machine

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -

    • Stress [N/m2 = Pa]

    • Strain [dimensionless]

    Stress and Strain:

    Tension and Compression Tests

    5

    By convention, a compressive

    force (thus, stress and strain) is

    taken to be negative

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -

    • Shear stress [N/m2 = Pa]

    • Shear strain [dimensionless]

    Stress and Strain:

    Shear and Torsional Tests

    6

    θ γ    tan=

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    ∴  Stress has units:

    N/m2 or lbf  /in2

    Engineering Stress

    • Shear  stress, τ :

     Area, Ao 

    F  t  

    F  t  

    F  s 

    F

    F

    F  s 

    τ  =F  s 

     A o 

    • Tensile stress, σ :

    original cross-sectional area

    before loading 

    σ  = F  t   A o 

    2f

    2mNor

    inlb=

     Area, Ao 

    F  t  

    F  t  

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    • Tensile strain: • Lateral strain:

    Strain is always

    dimensionless.

    Engineering Strain

    • Shear  strain:

    θ  

    90º

    90º - θ  y

    ∆ x γ  = Δ x /y  = tan θ  

    e = δ  Lo

     Adapted from Fig. 6.1 (a) and (c), Callister & Rethwisch 9e. 

    δ  /2 

    Lowo

    - δ  eL =

    wo

    δ  L /2 

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    • Simple tension: cable

    Note: τ  = M / Ac R  here.

    Common States of Stress

    o σ  =

    F  

     A 

    τ   =F  s 

     A 

    σ  σ  

    M  

    M  A o 

    2R  

    F  s  A c  

    • Torsion (a form of shear): drive shaftSki lift  (photo courtesyP.M. Anderson)

     A o = cross-sectional

    area (when unloaded) 

    F  F  

    τ  

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    (photo courtesy P.M. Anderson)Canyon Bridge, Los Alamos, NM 

    o σ  = F  

     A 

    • Simple compression:

    Note: compressivestructure member

    (σ  < 0 here).(photo courtesy P.M. Anderson)

    OTHER COMMON STRESS STATES (i)

     A o 

    Balanced Rock, ArchesNational Park 

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    • Bi-axial tension: • Hydrostatic compression:

    Pressurized tank

    σ   < 0h

    (photo courtesyP.M. Anderson)

    (photo courtesy

    P.M. Anderson)

    OTHER COMMON STRESS STATES (ii)

    Fish under water  

    σ  z   > 0

    σ  θ   > 0

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    2. Elastic Deformation

    • Elastic deformation is nonpermanent: when the applied load is released, the

    piece returns to its original shape (not breaking atomic bonds).

    • Hooke’s Law

    E [Pa]: Modulus of elasticity, or Young’s modulus

    12

    Linear elastic deformation Nonlinear elastic deformation

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 - 13

    Elastic means reversible!

    Elastic Deformation

    2. Small load

    F

    δ  

    bonds

    stretch 

    1. Initial 3. Unload

    return to

    initial 

    F

    δ  

    Linear-

    elastic 

    Non-Linear- elastic 

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 - 14

    Mechanical Properties• Slope of stress strain plot (which is proportional to the

    elastic modulus) depends on bond strength of metal

    Fig. 6.7, Callister & Rethwisch 9e. 

     Attraction

    Repulsion

    r 0

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -

    Elastic Deformation:

    Shear Stress and Strain• Elastic deformation is nonpermanent: when the applied load is released, the

    piece returns to its original shape.

    • Hooke’s Law

    G  [Pa]: Shear Modulus

    15

    • Shear stress [N/m2 = Pa]

    • Shear strain [dimensionless]

    θ γ    tan=

     

    θ 

    90º

    90º - θ y 

    ∆ x   

    γ = Δ x /y = tan θ 

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -

    Poisson's ratio, ν 

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     Axial (z) elongation (positive strain)

    and lateral (x and y) contractions

    (negative strains) in response to an

    imposed tensile stress

    • Relationship among elastic

    parameters for isotropic materials

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 - 17

    Poisson's ratio, ν  

    • Poisson's ratio, ν :

    Units:

    E : [GPa] or [psi]

    ν : dimensionless

    ν  > 0.50 density increases

    ν  < 0.50 density decreases(voids form)

    eL 

    e

    -ν  

    eν  = - L

    e

    metals: ν  ~ 0.33

    ceramics: ν  ~ 0.25

    polymers: ν  ~ 0.40

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -

    Table 6.1: Elastic and Shear

    Moduli and Poisson’s Ratio

    18

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 - 19

    Metals

     Alloys

    Graphite

    Ceramics

    Semicond

    PolymersComposites

    /fibers

    E (GPa)

    Based on data in Table B.2,

    Callister & Rethwisch 9e. 

    Composite data based on

    reinforced epoxy with 60 vol%

    of aligned

    carbon (CFRE),

    aramid (AFRE), or

    glass (GFRE)

    fibers.

     Young 

    s Moduli: Comparison

    109 Pa

    0.2

    8

    0.6

    1

    Magnesium, 

     Aluminum 

    Platinum 

    Silver, Gold 

    Tantalum 

    Zinc, Ti 

    Steel, Ni 

    Molybdenum 

    G raphite 

    Si crystal 

    Glass - soda 

    Concrete 

    Si nitride  Al oxide 

    PC 

    Wood( grain) 

     AFRE( fibers)  * 

    CFRE * 

    GFRE* 

    Glass fibers only 

    Carbon fibers only 

     A ramid fibers only 

    Epoxy only 

    0.4

    0.8

    2

    4

    6

    10

    20

    4 0

    6 08 0

    10 0

    200

    6008 00

    10 001200

    400

    Tin 

    Cu alloys 

    Tungsten 

     

     

    Si carbide 

    Diamond 

    PTF E 

    HDP E 

    LDPE 

    PP 

    Polyester  

    PS PET 

    C FRE( fibers) * 

    G FRE( fibers)* 

    G FRE(|| fibers)* 

     A FRE(|| fibers)* 

    C FRE(|| fibers)* 

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 -

    Summary

    1. Concept of stress and strain

    2. Mechanical testing: tensile, compression, shear and

    torsional tests

    3. Elastic deformation: Modulus of elasticity

    4. Poisson’s ratio

    21

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 - 22

    Linear Elastic Properties

    • Modulus of Elasticity, E :(also known as Young's modulus)

    • Hooke's Law:

    σ  = E  e σ  

    Linear-elastic 

    E  

    e

    F  

    F  simpletensiontest 

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 - 23

    • Elastic Shear

    modulus, G : 

    τ  

    G γ  

    τ  = G γ  

    Other Elastic Properties

    simple

    torsion

    test

    M  

    M  

    • Special relations for isotropic materials: 

    2(1 + ν )

    EG =

    3(1 - 2ν )

    EK =

    • Elastic Bulkmodulus, K: 

    pressure

    test: Init.vol =V o.

    Vol chg.

    = ΔV

    P  

    P   P  P  = -K  

     Δ VVo

    P

     Δ V

    K  Vo

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    MSE 3300 / 5300 UTA Spring 2015 Lecture 9 - 24

    • Simple tension: 

    δ  = FLoE Ao

    δ  L = - ν  Fw oE Ao

    • Material, geometric, and loading parameters all 

    contribute to deflection.

    • Larger elastic moduli minimize elastic deflection. 

    Useful Linear Elastic Relationships

    F  

     Aoδ  /2 

    δ  L /2 

    Lo wo

    • Simple torsion: 

    α  = 2MLoπ  ro

    4G

    M = momentα  = angle of twist 

    2r o 

    Lo