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Principle of lenear elastic fracture mechanicss
Typology: Study notes
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1
Type of Loading Modes
Stress Intensity Factor Approach
Experimental Determination of Fracture ToughnessFracture Toughness
Energy Balance Approach – StrainEnergy Release Rate
Limitation of LEFM and K-dominance
Case Studies
In deriving the solutions, there are twoalternative approaches:
the stress intensity/concentration approach, andand
the energy balance approach.
Both approaches are equivalent in certaincircumstances as demonstrated later inthe course
StressStress-
-intensity Approach
intensity Approach
Stress distribution near fillets in flat bar
When a structural member contain a discontinuity, such as hole or a sudden changein cross section, high localised stresses may occur near the discontinuity.
However the information are only useful for the specific design only
Hence the ratio of stress is used;
; Dimensionless, no unit
This ratio, K is referred stress concentration factor for the given discontinuity.
K may be computed once and for all in terms of ratios of the geometric parameters involved.
The results obtained may be expressed in the form of tables of graphs.
Stress distribution near circularhole in flat bar under axial loading.
Stress distribution near fillets in flat bar under axial load
loading.
Stress Concentration Factor (K)Stress Concentration Factor (K)
Example 2.1:Determine the largest axial load P that can be safely supported bya flat steel bar consisting of two portions both 10 mm thick andrespectively, 40 mm and 60 mm wide, connected by fillets of radiusr = 8 mm. Assume an allowable normal stress of 165 MPa.
Stress Concentration Factor (K)Stress Concentration Factor (K)
Cont’dCont’d
The presence of sharp corners, notches, or cracks serves to concentrate the appliedstress at these points.
Inglis showed, using elasticity theory, that the degree of stress magnification at theedge of the hole in a stressed plate depended on the radius of curvature of the hole.
The smaller the radius of curvature, the greater the stress concentration.
Inglis found that the “stress concentration factor”, K, for an elliptical hole is equalto:
........ Eq. 2.2a
c ρ
K
2
1
=
where c is the hole radius and
ρ
is the radius of
curvature of the tip of the hole.
For a very narrow elliptical hole, the stressconcentration factor may be very much greater thanone.
For a circular hole, Eq. 2.2a gives K = 3 (as shown inFig. 2.2.1). It should be noted that the stressconcentration factor does not depend on the absolutesize or length of the hole but only on the ratio of thesize to the radius of curvature.
sin
sin
cos
θ
θ
θ
π π
σ
σ
a r
x
z
z
x
y
cos
cos
sin
sin
sin
cos
θ
θ
θ
π π
σ
τ
θ
θ
θ
π π
σ
σ
π
r a r a^ r
xy
y
StressStress-
-intensity Factor (K)
intensity Factor (K)
Cont’dCont’d
I
a
C
K
I
π
σ
=
Example 2.2:Example 2.2:
Solution:Solution:
Critical StressCritical Stress-
-intensity Factor, K
intensity Factor, K
CC
All brittle materials contain a
population of small
cracks and flaws
that have a variety of sizes, geometries
and orientations.
When the magnitude of a tensile stress at the tip of oneof these flaws exceeds the value of this critical stress, acrack forms and then propagates, leading to failure.
Condition for crack propagation:
Condition for crack propagation:
If K becomes K
C
, then crack propagate.
K
IC
; plane strain fracture toughness; normally reported
as material property
Fracture toughness - good diagrams
http://www.ndt-ed.org/EducationResources/CommunityCollege/Materials/Mechanical/FractureToughness.htm
K
≥
K
c
Stress Concentration factor (Dimensionless)
Stress Intensity factor ( Pa.m
1/
/ Pa.√m)
ave
t
K
σ^ σ
max
=
Critical Stress Intensity factor or FractureToughness ( Pa.m
1/
/ Pa.√m)
a
K
π
σ
=
a
K
f
π
σ
=