IWSD 2012-M4_4 Design Against Brittle Fracture
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Transcript of IWSD 2012-M4_4 Design Against Brittle Fracture
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Objective: The student will be acquainted with brittle fracture analysis based on linear elastic fracture mechanics.
Module 4.4: Design against brittle fracture
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Scope: Fracture toughness, Critical stress intensity, Critical crack size, Temperature and material toughness Overview of calculation methods in a relevant design guidance document, e.g., EN 1993 Eurocode 3-part 1-10: Design of Steel Structures: Selection of materials for fracture toughness and through thickness properties
IWSD M4.4
Expected results: Review theory of fracture mechanics and brittle fracture. Explain relationship between material fracture toughness and temperature. Review calculation procedures in a relevant design guidance document. Compute critical crack size for structural element with typical material properties. Compute stress intensity factor for a welded connection.
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Brittle fracture
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Characterized by the failure occurs without prior plastic deformation
Some form of fracture is required (e.g. micro-cracks in a weld) to start the crack
A material that is ductile have less risk of brittle fracture.
Risk for brittle fracture when The stress level is high Low temperature Multi axial stress state (= large plate thickness) Stress concentrations
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Brittle fracture
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Brittle fracture in Liberty ships due to sudden decrease in temperature
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Impact Toughness
The steel used in the Titanic hull had adequate strength but low toughness in cold temperatures. When the Titanic hit the iceberg, instead of the steel bending and causing small cracks (ductile failure), a crack grew very fast and very large (due to brittle failure).
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Tensile testing stress strain diagram ductile material
10 mm
SEM photo of a ductile metal failure surface
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Tensile testing stress strain diagram brittle material
Fig 2.1 Stress-strain diagram for a typical brittle material.
10 mm
SEM photo of a brittle metal failure surface
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Impact Toughness
Depending on: Temperature Material thickness Chemical composition of the material The Structures design If there are notches in the structure If impact is precent Then the failure could either be ductile of brittle
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Impact Toughness testing
The toughness for a material is characterized by a Charpy V test The specimen, 10x10 mm in cross section, is impacted by a hammer and
the applied energy is registered as function of temperature
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Impact Toughness testing
Charpy V test: Measurement of the energy absorption in a notched specimen Rule of thumb: If the energy at service temperature 27 J the risk for
brittle failure is small Defines at which temperature (ITT) the test speicmens is failed at an
energy of 27 J (alt. 40, 50...) ITT = Impact Transition Temperature
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Impact toughness
Relation between transition temperature for impact toughness and lowest service temperature without risk for brittle failure for C- and CMn steels according to British Standard 4741
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Toughness
With regards to the risk for brittle fracture the steels are divided in different quality classes (toughness classes) from A to E where the highest requirements are E
General structural steels
SS EN 10027 -1:2005
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Choosing toughness class (BSK07/SS-EN 10025-2)
Toughness class is varying based on the risk for brittle fracture. It is determined according to this:
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Execution class (utfrandeklass) (BSK07/SS-EN 10025-2)
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Cutting class (skrklass) (BSK07/SS-EN 10025-2)
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Toughness
Besides the requirements for yield stress and ultimate strength, the material should fulfill three requirement regarding the thougness according to Eurocode 3
fuk/fyk 1,10
Elongnation 14%
u 15fyk/Ek
All the steels in the following tables fulfill these three requirements
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Excercise 4.4.1
IWSD M4.4
What toughness class is required for an un-alloyed steel S355 (SS-EN 10025-2) with the following conditions: Plate thickness 30 mm Lowest service temperature -30C Fatigue, but no impacts Joint class (frbandsklass) C = 50 Execution class (utfrande class) GB
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Chooice of toughness class (Eurocode 3)
One reference temperature is determined
IWSD M4.4
= Lowest design temperature (EN 1991-1-5). Given for all Swedish cities
= Radiation loss (= 0, EN 1991-1-5).
= Adjustment for geometry, design and material (could be set to = 0 if table 2.1 is used)
= Extra safety margin (normally = 0)
= Adjustment if the strain rate is higher than , see next page
= Adjustment for cold forming, see next page
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Chooice of toughness class (Eurocode 3)
Adjustment for strain rate other than:
which is base for table 2.1
This could for instance be impacts where the real strain rate is known
fy(t) = the materials yield strength as function of the plate thickness
When cold forming
where cf= is the cold forming grade in %
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Chooice of toughness class (Eurocode 3)
Ed= External design stress fy(t) = the materials yield strength as function of the plate thickness
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Crack growth of macro cracks
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Region 1: Threshold
Depends on the R-ration
For welds Kth = 2 MPam
Region 2: Linear stable crack growth
a = crack length N = number of cycles da/dN = crack growth/cycle K = SIF range C and n are material dependent constants
Paris law
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Region 3: Instability final failure
Fracture toughness Kc depends on: Material quality (increases with increase quality) Thickness (decrease with increased thickness) Temperature (decrease with lower temperature)
Threshold region Paris region
Instability region
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Region 3: Instability final failure
Fracture toughness Kc
Plane stress Transition area Plane strain
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Fracture toughness Kic testing
CT-specimen
3 point bending
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Fracture toughness Kic testing
The test is carried out in two stages: First stage is fatigue to develop a fatigue crack. The crack length is
determined after the fatigue test (0.45W < a < 0.55W) A slowly increased load P is applied. The Crack tip Opening
Displacement (COD) is measured and plotted vs. P.
Tensile test, CT (Compact Tension)
Bending test
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Fracture toughness Kic testing
Stress intensity factor - CT
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Fracture toughness Kic testing
Stress intensity factor 3 pt bending
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Stress Intensity Factor, SIF
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aSK yC
Kc is a material parameter called the critical stress intensity factor or fracture toughness
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Apporximative relation between impact toughness and fracture toughness According to SSAB
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KV = Impact toughness according to charpy V testing in Joule
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Problem 4.4.1
Change to a High Strength Steel Assume that a component in the shape of a large sheet is to be fabricated C-Mn Steel. It is required that the critical flaw size be greater than 2 mm, the resolution limit of available flaw detection procedures. A design stress of one half the tensile strength is indicated. To save weight, and increase in the tensile strength is suggested, from 1520 to 2070 MPa. Is such a strength increment allowable ? (assume plane-strain conditions in all computations)
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