How Inspectors Can Use Fracture Mechanics Roger Cordes

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    How Inspectors Can UseFracture Mechanicsby Roger Cordes, Ph.D., P.E.

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    Roger Cordes, Ph.D., P.E.

    Involved with a wide variety of solid mechanics projectsfor SES Floating Production Systems and Fitness-For-Service groups.

    Generally focused on solid mechanics analyses includingstrength and fatigue assessments.

    Involved in contact problems, damage evolution,dynamic/impact simulations, post-buckling behavior,thermal behavior, and crack modeling.

    Crack assessment projects at SES include prediction ofcrack growth rates and component life, maximumacceptable initial flaw size studies, and forensic work.

    B.S.M.E from the University of Arkansas and a Ph.D.from Northwestern University. Licensed ProfessionalEngineer in Texas.

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    Purpose of Presentation: Discussing howfracture models can be used in conjunctionwith inspections

    Overview Typical analyses Basic fracture mechanics Material toughness and critical crack sizes Fatigue crack growth and ECAs Inputs needed and safety factors

    Sources API 579 Fitness for Service British Standard 7910 Guide to Methods for

    Assessing the Acceptability of Flaws in MetallicStructures

    API 1104 Welding of Pipelines and RelatedFacilities

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    Overview

    Relating fracture mechanics to inspections

    Typical analyses

    Basic fracture mechanics

    Material toughness and critical crack sizes

    Fatigue crack growth and ECAs

    Inputs needed and safety factors

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    Typical Analysis

    A Stress Analysis of a Pipe,Vessel, Component

    Stresses

    Can it survive theloading?

    How long is it predictedto last?

    (Strength Check) (Fatigue Check)

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    How Fracture Mechanics Fits In

    A Stress Analysis of a Pipe,Vessel, Component

    Stresses

    How big a crack cansurvive the loading?

    How fast will a crackgrow?

    How big an initialcrack is OK?

    (Flaw tolerance/Toughness Check)

    (Inspection Interval Check)

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    Nomenclature

    Inspectors find indications.If the indication is larger than a pre-defined

    acceptable size, it is a defect.

    If the indication is sharp, it is a crack.

    Crack

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    The Basics of Fracture Mechanics (1)

    s

    If you pull on something with avoid or particle in it, you get a

    stress concentration factor(SCF).

    If you flatten that void,you get a crack with astress intensity factor

    (K).

    s

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    The stress field at the tip of the crack can bewritten in the following form:

    s is the far field stress,

    Y is a function of the geometry,

    ais the crack length, and

    Kis the stress intensity factor.

    a

    r

    s

    The Basics of Fracture Mechanics (2)

    aYK s

    MATERIAL

    MATERIAL

    KK

    KK

    2 Options

    Failure not predicted

    Failure predicted

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    Fracture Toughnesses

    Material

    Approximate Values

    Charpy

    (ft-lbs)

    CTOD (mm) KMATERIAL(ksi*in.)

    Glass

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    Surface Crack Example

    0.00

    0.10

    0.20

    0.30

    0.40

    0.50

    0.60

    0.70

    0.80

    0.90

    0.0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0

    Crack Length, inches

    CrackDepth,

    in

    ches

    .

    Case A

    Case B

    Case C

    Wall Thickness

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    Fatigue Crack Growth

    Cracks mainly grow from the stress rangeduring cyclic loading.

    High

    Stress

    LowStress

    StressRange

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    Crack Growth

    OD Surface Crack Depth Growth versus Time

    0.0

    2.0

    4.0

    6.0

    8.0

    10.0

    12.0

    14.0

    0.0 3.0 6.0 9.0 12.0 15.0

    Time, years

    CrackDepth,m

    m

    Initial Height = 1.0 mm

    Initial Height = 1.5 mm

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    Crack Growth Over Time

    Final crack

    width, 2Cf

    Initial crack

    width, 2CiInitial crackdepth, ai

    Final crack

    depth, af

    ECA=Engineering Critical AssessmentCommonly used to determine the initialcracksizes that are OK based on the expectedloading over the life of the component.

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    ECA Results

    0.00

    0.02

    0.04

    0.06

    0.08

    0.10

    0.12

    0.14

    0.16

    0.00 0.25 0.50 0.75 1.00 1.25 1.50 1.75 2.00

    Crack Width, 2C (inches)

    CrackDepth,a(inches)

    .

    Proposed Criteria

    ECA Result

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    Crack Locations and Orientations

    Acceptable crack criteria can be define for

    Circumferential cracks driven by axial stress

    Axial cracks driven by hoop stress

    Internal Surface Crack

    External Surface Crack

    Wall

    Thickness

    Embedded

    Crack

    Inner

    Radius

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    Interaction Rules

    If cracks are too close together, they

    are treated as one crack.

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    API 579 Fitness for Service and

    British Standard 7910

    Failure assessment diagram (FAD) approach

    is used for the ECA (API 579) and BS7910.

    FAD based on

    K

    Plastic

    Collapse

    FAD

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    Inputs for Analysis

    Significant inputs driving the solution:

    Geometry

    SCF

    Primary Cyclic Loading

    Crack Growth Constants

    Target Life

    Initial Crack Size

    Material Toughness

    Other inputs

    Residual Stress

    Maximum Primary Stress

    Yield/Ultimate Strengths

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    Safety Factors

    API 579 utilizes safety factors on three items:

    Applied Loading

    Fracture Toughness

    Crack Size

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    How Fracture Mechanics Fits In

    Before Putting aComponent in Operation

    Do Fracture MechanicsEvaluation

    Determine Allowable FlawSizes for Life of Vessel

    Set Inspection Criteria

    If You Inspect and Find aCrack During Operation

    Do Fracture MechanicsEvaluation

    See How Big Crack Can Get

    Or

    See How Fast Crack Will Grow

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    Questions ???

    Roger Cordes, Ph.D., P.E.Stress Engineering Services, Inc.

    13800 Westfair East DriveHouston, Texas 77041-1101

    Phone: 281-955-2900Fax: 281-955-2638

    Email: [email protected] Site: www.stress.com

    mailto:[email protected]://www.stress.com/http://www.stress.com/mailto:[email protected]