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  • 8/11/2019 Lecture02 Slides ME382 UofM

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    ME 382

    Lecture 02

    Suggested Reading:

    A&J-1: 8 (not 8.8); 11.4

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    3 Important Terms for Mechanical Design

    Stiffness

    Strength

    Toughness

    How arethese

    different?

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    Tensile test to measure mechanical properties

    lo

    P

    P

    cross sectionalarea Ao

    1. Measure length and area

    2. Pull specimen

    Measure load, P

    Measure extension, !

    But, this curve depends on your choice of specimen .

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    Engineering (nominal) stress and strain

    Engineering (nominal) stress: !n = P /Ao

    (Aois original cross sectional area)

    Engineering (nominal) strain: "n = #/ lo(lois original length)

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    Nominal stress-strain curve for a ductile metal

    Nominal stress (MPa)

    Nominal strain

    X

    neckingbegins

    (ultimate)

    tensile strength

    yield strength(yield stress)

    (onset of plasticity)

    yield begins

    linear elastic deformation

    (slope =modulus)

    plastic deformation

    (movement of dislocations)

    fracture

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    Other mechanical properties

    Measures of ductility:Percent elongation:

    Reduction in area:

    100!lf - l0

    l0

    Energy absorption: U= Pd"#

    Energy

    per unit volume:u = "nd#n$(area under stress strain curve)

    (J)

    (Jm-3)

    100!A

    0- A

    break

    A0

    100!10mm- 5mm

    5mm=100%

    100!10mm- 7mm

    7mm= 42.9%

    100!10mm

    2- 5mm

    2

    10mm2

    = 50%

    100!10mm

    2- 7mm

    2

    10mm2

    = 30%

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    Unloading

    Permanent deformation after yield

    Note - not the

    same slope for

    1&2 unless its atrue stress-true

    strain curve.

    Why?

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    True Stress and True Strain

    After yield, memoryof original shape is lost

    $nominal stress and strain may be meaningless

    True strain: d"= dl

    l

    lis current length

    True stress: "=P

    AAis current area

    "="n1+ #

    n

    ( )

    "= ln 1+ "

    n( )

    (if volume is conserved)

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    Work hardening (strain hardening) results in an increase inyield strength - cold work

    Often described by power-lawhardening: "= H#n

    True stress / true strain tensile curve

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    Experimental data for a 5754 aluminum alloy

    0

    50

    100

    150

    200

    250

    0 0.05 0.1 0.15 0.2

    5754 Aluminum alloy

    Truestress(M

    Pa)

    True strain

    "= H#n

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    1

    10

    100

    1000

    0.001 0.01 0.1

    5754 Aluminum alloy

    Truestress(MP

    a)

    True strain

    != 367 "0.238~ ~

    Determining the strain-hardening parameters

    !! = H!!n

    ln !! = n ln!!+ lnH

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    0

    50

    100

    150

    200

    250

    0 0.02 0.04 0.06 0.08 0.1

    5754 Aluminum alloy

    Truestress(MP

    a)

    True strain

    power law

    experimental data

    Comparison of power-law with experimental results

    Pretty good!

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    There are other forms of uniaxial stress-strain curves.