mom chapter 3-mechanical properties of materials

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  • 7/29/2019 MOM Chapter 3-Mechanical Properties of Materials

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    Chapter Objectives Understand how to measure the stress and strain

    through experiments

    Correlate the behavior of some engineering materials

    to the stress-strain diagram.

    Copyright 2011 Pearson Education South Asia Pte Ltd

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    1. Check homework, if any

    2. Reading Quiz

    3. Applications

    4. Stress-Strain diagram5. Strength parameters

    6. Poissons ratio

    7. Shear Stress-strain diagram

    8. Concept Quiz

    In-class Activities

    Copyright 2011 Pearson Education South Asia Pte Ltd

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    TENSION AND COMPRESSION TEST

    Copyright 2011 Pearson Education South Asia Pte Ltd

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    READING QUIZ

    1) The modulus of elasticity E is a measure ofthe linear relationship between stress and

    strain. The common unit is:

    a) kN/mm2

    b) MPa

    c) GPa

    d) All of them

    Copyright 2011 Pearson Education South Asia Pte Ltd

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    READING QUIZ (cont)

    2) The Poissons ratio, vof commonengineering materials lies in the range:

    a) 0 v 1

    b) 0 v 0.5

    c) -1 v 1

    d) -0.5 v 0.5

    Copyright 2011 Pearson Education South Asia Pte Ltd

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    APPLICATIONS

    Copyright 2011 Pearson Education South Asia Pte Ltd

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    APPLICATIONS (cont)

    Copyright 2011 Pearson Education South Asia Pte Ltd

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    STRESS STRAIN DIAGRAM

    Copyright 2011 Pearson Education South Asia Pte Ltd

    Note the critical status for strength specification

    proportional limit

    elastic limit

    yield stress

    ultimate stress

    fracture stress

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    STRENGTH PARAMETERS

    Copyright 2011 Pearson Education South Asia Pte Ltd

    Modulus of elasticity (Hookes Law)

    Modulus of Resistance

    Modulus of Toughness

    It measures the enter areaunder the stress-strain diagram

    E

    Eu plplplr

    2

    21

    21

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    EXAMPLE 1

    Copyright 2011 Pearson Education South Asia Pte Ltd

    The stressstrain diagram for an aluminum alloy that is used

    for making aircraft parts is shown in Fig. 319. If a specimen

    of this material is stressed to 600 MPa, determine the

    permanent strain that remains in the specimen when the load

    is released. Also, find the modulus of resilience both before

    and after the load application.

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    EXAMPLE 1 (cont)

    Copyright 2011 Pearson Education South Asia Pte Ltd

    When the specimen is subjected to the load, the strain is approximately

    0.023 mm/mm.

    The slope of line OA is the modulus of elasticity,

    From triangle CBD,

    Solutions

    mm/mm008.0

    100.7510600 9

    6

    CDCDCD

    BDE

    GPa0.75

    006.0

    450E

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    EXAMPLE 1 (cont)

    Copyright 2011 Pearson Education South Asia Pte Ltd

    This strain represents the amount ofrecovered elastic strain.

    The permanent strain is

    Computing the modulus of resilience,

    Note that the SI system of units is measured in joules, where 1 J = 1 N

    m.

    Solutions

    (Ans)MJ/m40.2008.060021

    2

    1

    (Ans)MJ/m35.1006.04502

    1

    2

    1

    3

    3

    plplfinalr

    plplinitialr

    u

    u

    (Ans)mm/mm0150.0008.0023.0 OC

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    POISSONs RATIO

    Copyright 2011 Pearson Education South Asia Pte Ltd

    long

    latv

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    EXAMPLE 2

    Copyright 2011 Pearson Education South Asia Pte Ltd

    A bar made of A-36 steel has the dimensions shown in Fig.

    322. If an axial force of P = 80kN is applied to the bar,

    determine the change in its length and the change in the

    dimensions of its cross section after applying the load. The

    material behaves elastically.

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    EXAMPLE 2 (cont)

    Copyright 2011 Pearson Education South Asia Pte Ltd

    The normal stress in the bar is

    From the table for A-36 steel, Est= 200 GPa

    The axial elongation of the bar is therefore

    Solutions

    mm/mm108010200

    100.16 66

    6

    st

    zz

    E

    Pa100.1605.01.0

    1080 63

    A

    Pz

    (Ans)m1205.11080 6z zz L

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    EXAMPLE 2 (cont)

    Copyright 2011 Pearson Education South Asia Pte Ltd

    The contraction strains in both thexand ydirections are

    The changes in the dimensions of the cross section are

    Solutions

    m/m6.25108032.0 6 zstyx v

    (Ans)m28.105.0106.25

    (Ans)m56.21.0106.25

    6

    6

    yyy

    xxx

    L

    L

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    SHEAR STRESS-STRAIN DIAGRAM

    Copyright 2011 Pearson Education South Asia Pte Ltd

    Strength parameter G Shear modulus of elasticity or the

    modules of rigidity

    G is related to the modulus of elasticity E and Poissonsratio v.

    G

    vE

    G

    12

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    EXAMPLE 3

    Copyright 2011 Pearson Education South Asia Pte Ltd

    A specimen of titanium alloy is tested in torsion and the

    shear stress strain diagram is shown in Fig. 325a.

    Determine the shear modulus G, the proportional limit, and

    the ultimate shear stress. Also, determine the maximum

    distance dthat the top of a block of this material, shown in

    Fig. 325b, could be displaced horizontally if the material

    behaves elastically when acted upon by a shear force V.What is the magnitude ofV necessary to cause this

    displacement?

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    EXAMPLE 3 (cont)

    Copyright 2011 Pearson Education South Asia Pte Ltd

    By inspection, the graph ceases to be linear at pointA. Thus, the

    proportional limit is

    This value represents the maximum shear stress, point B. Thus the

    ultimate stress is

    Since the angle is small, the top of

    the will be displaced horizontally by

    Solutions

    (Ans)MPa504u

    (Ans)MPa360pl

    mm4.0mm50

    008.0rad008.0tan dd

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    EXAMPLE 3 (cont)

    Copyright 2011 Pearson Education South Asia Pte Ltd

    The shear force Vneeded to cause the displacement is

    Solutions

    (Ans)kN2700

    10075MPa360; V

    V

    A

    Vavg

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    CONCEPT QUIZ

    1) The head H is connected to the cylinder of acompressor using six steel bolts. If the

    clamping force in each bolt is 4000N,

    determine the normal strain in the bolts.

    Each bolt has a diameter of 5 mm. Ify= 280

    MPa and Est = 210GPa, what is the strain ineach bolt when the nut is unscrewed so that

    the clamping force is released?

    Copyright 2011 Pearson Education South Asia Pte Ltd

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    CONCEPT QUIZ (cont)

    a) 0.970

    b) 0.203

    c) 0.970(10-3)

    d) Insufficient information to

    determine because the

    stress is beyond yield point

    Copyright 2011 Pearson Education South Asia Pte Ltd