stress concentration
DESCRIPTION
njTRANSCRIPT
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VIT University
Semester:- Fall, 2010-2011
Unit-I
Presented by
Prof.E.RAJ KUMAR
Prof.E.Raj kumar, Design Division, SMBS
Design of Machine Element (MEE302)
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Prof.E.Raj kumar, Design division, SMBS 2
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Prof.E.Raj kumar, Design division, SMBS 3
WHY STUDY Failure?
The engineer has to minimize the possibility of failure since the design step.
Understand the mechanics of the various failure modes
fracture, fatigue, and creep
Be familiar with appropriate design principles to prevent in-service failures.
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Prof.E.Raj kumar, Design division, SMBS 4
Fracture
In response to an imposed stress, any fracture process involves two steps:
crack formation
and propagation.
The mechanism of crack propagation determine the mode of fracture.
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Prof.E.Raj kumar, Design division, SMBS 5
Ductile Fracture
Ductile fracture: extensive plastic deformation in the vicinity of an
advancing crack.
proceeds relatively slowly as the crack length is extended.
often said as stable crack. it resists any further extension unless there is an increase in
the applied stress.
Normally there will be evidence of appreciable gross deformation at the fracture surfaces (e.g., twisting and tearing).
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Prof.E.Raj kumar, Design division, SMBS 6
Ductile Fracture
Highly ductile fracture in
which the specimen necks down to a point.
Moderately ductile
fracture after some necking.
Brittle fracture
without any plastic deformation.
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Prof.E.Raj kumar, Design division, SMBS 7
Ductile Fracture
Normal fracture process stages: necking
formation of small cavities (microvoids) in the interior of the cross section,
as deformation continues, these microvoids enlarge, come together, and to form an elliptical crack,
which has its long axis perpendicular to the stress direction.
The crack continues to grow in a direction parallel to its major axis by this microvoid coalescence process.
Finally, fracture occurs by the rapid propagation of a crack around the outer perimeter of the neck, by shear deformation at an angle of about 45
with the tensile axis
this is the angle at which the shear stress is a maximum.
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Prof.E.Raj kumar, Design division, SMBS 8
(a) Initial necking.
(b) Small cavity formation.
(c) Coalescence of cavities to form a crack.
(d) Crack propagation.
(e) Final shear fracture at a 45
angle relative to the tensile direction.
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Prof.E.Raj kumar, Design division, SMBS 9
The magnitude of the localized stress diminishes with distance away from the crack tip.
At positions far removed, the stress is just the nominal stress.
Due to their ability to amplify an applied stress in their locale, these flaws are sometimes called stress raisers.
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Prof.E.Raj kumar, Design division, SMBS 10
Concept of Stress Concentration
Theoretical stress
concentration factor, Kt
Maximum stress at the discontinuity
Nominal stress, max stress
with no discontinuity
Kt is used for normal
stresses and Kts for
shear stresses.
In a machine element, if there is a discontinuity such as sudden change in cross
section, a fillet Hole,groove or notch;highly localised stresses are induced at such
places. Such discontinuities are called stress raisers and the localised stress
effect they produce is termed as stress concentration.
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Prof.E.Raj kumar, Design division, SMBS 11
Concept of Stress Concentration
Consider an elliptical hole in an infinitely large plate loaded in uniform
tension. Using the theory of elasticity the theoretical stress concentration
factor is given by the equation below.
Elliptical hole
2b
2a
For a circular hole Kt = 3
The equation can be applied to a longitudinal crack where b
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Prof.E.Raj kumar, Design division, SMBS 12
Stress Concentration Factor
Stress concentration factor is found using experimental methods.
Photoelasticity a plane polarized light is passed thru a photelastic material (all transparent plastics) resulting in a
colorful fringe pattern indicating the intensity of the stress.
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Prof.E.Raj kumar, Design division, SMBS 13
Stress Concentration Factor
Brittle Coating a specially prepared lacquers are usually
applied by spraying on the actual
part. After air drying, the part is
subjected to stress. A pattern of
small cracks appear on the surface.
Data could be used to locate strain
gages for precise measurement of
the stress. The method is sensitive
to temperature and humidity.
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Prof.E.Raj kumar, Design division, SMBS 14
Stress Concentration Factor
Electrical strain gauges
The method is the most popular and widely accepted for strain measurements and
stress analysis. The strain gauge consists of a grid of strain-sensitive metal foil
bonded to a plastic backing material. When the gauge is subjected to a mechanical
deformation, its electrical resistance changes proportionally. The change in voltage
is converted to strain and the stress is calculated from the strain.
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Prof.E.Raj kumar, Design division, SMBS 15
Stress Concentration Factor
Finite Element method
The CAD model is subdivided into many small pieces of simple
shapes called elements.
FEA program writes the equations governing the behavior of each
element taking into consideration its connectivity to other elements.
These equations relate the unknowns, for example displacements in
stress analysis, to known material properties, restraints and loads.
The program assembles the
equations into a large set of
simultaneous algebraic
equations (thousands or even
millions).
These equations are then
solved by the program to
obtain the stress distribution
for the entire model.
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Prof.E.Raj kumar, Design division, SMBS 16
Stress Concentration Factor
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Prof.E.Raj kumar, Design division, SMBS 17
Stress Concentration Factor
Round section
with a fillet
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Prof.E.Raj kumar, Design division, SMBS 18
Stress Concentration Factor
Flat plate
with a hole
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Prof.E.Raj kumar, Design division, SMBS 19
IMPACT FRACTURE TESTING
Two standardized tests were designed to measure the impact energy (notch toughness): Charpy (commonly used in the USA)
Izod.
One of the primary functions is to determine whether or not a material experiences a ductile-to-brittle transition with decreasing temperature. If so, what is the range of temperatures over which it
occurs.
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Prof.E.Raj kumar, Design division, SMBS 20
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Prof.E.Raj kumar, Design division, SMBS 21
, =Impact stress induced
l E
l s
x d
= =
Fl h W 2
1 ) ( = + d
l
AE F
d =
A F s =
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Prof.E.Raj kumar, Design division, SMBS 22
Temperature dependence of the Charpy V-notch impact energy (curve A) and percent shear fracture (curve B) for an A283 steel.
AL
UE 2 = s
Al
EG 4 = t
Impact Tension
Impact Torsion
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Prof.E.Raj kumar, Design division, SMBS 23
IMPACT FRACTURE TESTING
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Prof.E.Raj kumar, Design division, SMBS 24