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4/10/2012 1 Fatigue Failure Criteria By Soheil Nakhodchi Machine Element Design I K.N.Toosi University of Technology 1 Chapter 6 - Outline 2 6–1 Introduction to fatigue in metals 6–2 Approach to fatigue failure in analysis and design 6–3 Fatigue life methods 6–4 The stress-life method 6–5 The strain-life method 6–6 Linear elastic fracture mechanics method 6–7 The endurance limit 6–8 Fatigue strength 6–9 Endurance limit modifying factor 6–10 Characterizing fluctuating stresses 6–11 Torsional fatigue stress strength under fluctuating stress 6–12 Combination of loading modes 6–13 varying, fluctuating stress, cumulative fatigue damage Fatigue failure criteria for fluctuating stress 3 It has midrange stress plotted along the abscissa and all other components of stress plotted on the ordinate, with tension in the positive direction. The endurance limit, fatigue strength, or finite-life strength whichever applies, is plotted on the ordinate above and below the origin. The midrange line is a 45 o line from the origin to the tensile strength of the part. Figure 7-24 Modified Goodman diagram showing all the strengths and the limiting values of all the stress components for a particular midrange stress 4 Plot of Fatigue Failures for Midrange Stresses in both Tensile and Compressive Regions.

Chapter 6 - Outline Machine Element Design I · Machine Element Design I K.N.Toosi University of Technology 1 Chapter 6 - Outline 2 6–1 Introduction to fatigue in metals 6–2 Approach

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  • 4/10/2012

    1

    Fatigue Failure Criteria

    By

    Soheil Nakhodchi

    Machine Element Design I

    K.N.Toosi University of Technology

    1

    Chapter 6 - Outline

    2

    6–1 Introduction to fatigue in metals6–2 Approach to fatigue failure in analysis and design6–3 Fatigue life methods6–4 The stress-life method 6–5 The strain-life method 6–6 Linear elastic fracture mechanics method6–7 The endurance limit6–8 Fatigue strength 6–9 Endurance limit modifying factor 6–10 Characterizing fluctuating stresses6–11 Torsional fatigue stress strength under fluctuating stress 6–12 Combination of loading modes6–13 varying, fluctuating stress, cumulative fatigue damage

    Fatigue failure criteria for fluctuating stress

    3

    It has midrange stress plotted along the abscissa and

    all other components of stress plotted on the

    ordinate, with tension in the positive direction.

    The endurance limit, fatigue strength, or finite-life

    strength whichever applies, is plotted on the

    ordinate above and below the origin.

    The midrange line is a 45o line from the origin to the

    tensile strength of the part.

    Figure 7-24

    Modified Goodman diagram showing all the strengths and

    the limiting values of all the stress components for a

    particular midrange stress

    4

    Plot of Fatigue Failures for Midrange Stresses in both Tensile and Compressive Regions.

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    5

    Master curve for fatigue

    Figure 7-26

    Master fatigue diagram for AISI 4340 steel with Sut= 158 Sy = 147 kpsi.

    The stress component at Aare

    σmin = 20, σ max = 120, σ m = 70, σ o = 50

    all in kpsi

    Fluctuating Stresses

    Failure data for Sm in tension and in compressionCOMPRESSIVE mean stresses are BENEFICIAL (or have no effect) in fatigue TENSILE mean stresses are DETRIMENTAL for fatigue behavior

    S is for strength

    2. Representing mean stress effect using modified Goodman Diagram

    Mean Stress Effect (R -1)

    Various curve of failure

    7

    FAILURE CRITERIA (mean stress)

    8

    B

    1- Modified Goodman Theory (Germany, 1899)

    1a me u

    S SS S

    Factor of Safety

    Load Line slope

    a

    m

    SrS

    1a me uS S n

    n = OA/OB

    For infinite life Failure Occurs When:

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    9

    B C

    D E

    F

    n = OC/OB

    2- The Soderberg Theory (USA, 1933)

    1a me y

    S SSS

    Factor of SafetyFor infinite life Failure Occurs When:

    For finite life fatigue

    strength Sf = areplaces Se

    1a me yS S n

    FAILURE CRITERIA (mean stress)

    10For finite life σa replaces Se

    3- The Gerber Theory (Germany, 1874)

    Factor of Safety

    B C

    D E

    F

    2

    1maue

    SS

    SS

    2

    1a me u

    n nS S

    n = OF/OB

    Failure Occurs When:

    Factor of Safety

    FAILURE CRITERIA (mean stress)

    11

    Factor of Safety

    B CD E

    F

    22

    1a me y

    S SS S

    2 2

    1a me

    n nS Sy

    n = OE/OB

    4- The ASME Elliptic

    Failure Occurs When:

    FAILURE CRITERIA (mean stress)

    12

    Factor of Safety

    B CD E

    F

    22

    1a me y

    n nS S

    n = OE/OB

    Failure Occurs When

    22

    1a me y

    S SS S

    4- The ASME Elliptic

    FAILURE CRITERIA (mean stress)

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    13

    5- The Langer (1st Cycle) Yield Line

    Failure Occurs When

    Factor of Safety

    1a myt ytS S n

    n = OD/OBB C

    D E

    F

    1y

    a

    yt t

    mS SSS

    FAILURE CRITERIA (mean stress)

    14

    Criteria Equations(7-43)

    (7-44)

    (7-45)

    (7-46)

    (7-47)

    15 16

    The stresses nσa and nσm can replace Sa and Sm, where n is the design factor or factorof safety.Then, Eqs. (7-43) to (7-46) become:

    (7-48)

    (7-49)

    (7-50)

    (7-51)

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    17

    We will emphasize the Gerber and ASME-elliptic for fatigue failure criterion and the Langer for first-cycle yielding. However, conservative designers often use the modified Goodman criterion. The design equation for the Langer first -cycle-yielding is

    The failure criteria are used in conjunction with a load line, Principal intersections are tabulated in Tables 7-9 to 7-11. Formal expressions for fatigue factor of safety are given in the lower panel of Tables 7-9 to 7-11. The first row of each table corresponds to the fatigue criterion, the second row is the static Langer criterion, and the third row corresponds to the intersection of the static and fatigue criteria.

    (7 *)

    18

    TABLE (7-9)Amplitude and Steady Coordinates of Strength and Important Intersections in First Quadrant for Modified Goodman and Langer Failure Criteria.

    FatigueCriterion

    Static Langer Criterion

    Intersection of the Static and Fatigue Criteria

    19

    TABLE (7-11)

    Amplitude and Steady Coordinates of Strength and Important Intersections in First Quadrant for ASME Elliptic and Langer Failure Criteria.

    ASME Elliptic

    Langer

    Intersection of ASME Elliptic and Langer

    Special Cases of Fluctuating Stresses

    20

    • Case 1: m fixed

    • Case 2: a fixed

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    Special Cases of Fluctuating Stresses

    21

    • Case 3: a / m fixed

    • Case 4: both vary arbitrarily

    22

    EXAMPLE 7-11 (Textbook)

    Solution

    (7-18) (7-4), p. 329

    23

    EXAMPLE 7-11 (Textbook)

    (7-25), p. 331

    (7-8), (7-17), p. 325, p. 328

    (7-10)

    24

    (7-*)

    (7-28)

    (7-10)

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