Metals Flashcards
(46 cards)
How can strength be defined?
resistance of a material to fracture
or resistance of a material to plastic flow
How can toughness be defined?
resistance to the propagation of a crack. E.g a crack will reduce the cross section and therefore increase the stress for an applied load. A tough material will yield and plastically deform = work hardening and energy will be absorbed. If the material is not tough the crack will propagate, little energy will be absorbed and fracture will then occur as applied stress level are far below yield strength.
Compare brittle vs ductile fracture
1.Deformation Before Fracture
Ductile: Significant plastic deformation
Brittle: Little or no plastic deformation
2.Warning Signs
Ductile: Necking & elongation before failure
Brittle: Sudden failure without warning
3. Energy Absorption (Toughness)
Ductile: High energy absorption
Brittle: Low energy absorption
4. Fracture Surface
Ductile: Rough, fibrous, cup-and-cone shaped
Brittle: Smooth, flat, cleavage or granular
5. Crack Propagation
Ductile: Slow, with plastic blunting
Brittle: Fast, unstable crack growth
7. Stress-Strain Graph Shape
Ductile: Curve with yield point, plastic region, and necking
Brittle: Linear elastic until sudden fracture
What are the 3 main modes of brittle failure?
Cleavage failure
Intergranular failure
What is cleavage failure?
only failure mode in completely brittle materials, but can occur in
normally ductile materials under certain conditions.
* In cleavage fracture, the crack path is transgranular, i.e. it passes through the grains.
* The crack propagates by breaking atomic bonds on a specific
crystallographic planes – normally the most densely packed atomic planes.
* The cleavage plane is normally the {001} plane in BCC materials, such as Fe, Mo, W etc.
* The steps/ridges within a grain are due to small changes in the local
misorientations in the grain, which can change the cleavage plane.
* The crack path will divert on crossing a grain boundary in a polycrystalline material.
What is intergranular failure?
Intergranular failure typically occurs when detrimental impurities
(P, As, S etc.) segregate to grain boundaries in polycrystalline
materials. The fracture surface is characterised by a granular
structure showing the individual grains.
The impurities reduce the cohesion between the grains, so the
grains separate with little or no plastic deformation (even if
the individual grains are very ductile)
What does the transition from cleavage to intergranular fracture depend on?
Depends on the ratio of the grain boundary energy to the energy of the surface exposed by cleavage.
What can suppress intergranular failure?
predicted in many pure metals but the segregation of beneficial impurities suppress intergranular failure
How do plastics Zones form?
materials that are able to plastically deform above their yield strength, i.e. most metals, a zone of plastic
deformation is formed ahead of the crack tip. In the plastic region, voids develop and grow, absorbing energy. This localised plastic deformation blunts the crack and the stress concentrating effect is less severe than in a brittle material.
This zone forms where the stress exceeds the yield strength of the material.
What is the size of the plastic zone determined by?
The size of the plastic zone can be determined by solving the distance from the crack tip when the stress is equal to the yield stress.
What causes a jagged ductile failure in metal alloys?
Most engineering materials contain small particles (carbides, oxides, nitrides etc.) which act as stress
concentrators.
These can separate from the matrix
(decohesion) or fracture depending on the strength of the matrix. This results in an internal crack at the centre of the necked region on a plane normal to the applied tensile axis.
The nucleated voids formed then grow and join up as the crack advances until final fracture.
What is ductile dimpling?
The fracture surface
associated with a ductile
fracture in a metal is
characterised by ‘ductile
dimpling’ where the small
particles have separated
from the matrix. Final failure occurs at shear.
Compare brittle fracture and ductile failure mechanisms in summary.
- Brittle fracture occurs via a cleavage or intergranular fracture
mechanism with very little plastic deformation and little energy
absorbed. - Ductile failure is associated with plastic deformation leading to
void formation and coalescence at the crack tip, which blunts
the crack and absorbs energy.
What is fatigue?
Occurs under dynamic rather than static stresses, after a long period of time by slow growth of crack under fluctuating stress. Can oocure without warning with limited plastic deformation which would shown impending failure.
What are the 3 factors required for fatigue failure?
*A tensile stress of sufficiently high value.
*A large fluctuation in the applied stress.
*A large enough number of cycles to the applied stress.
What variables can control/ alter the fatigue behaviour?
- Stress concentration
- Temperature
- Microstructure
- Residual stress
- Environment
What are the 3 main cyclic stresses applied to create failure?
1.Completely reversed stress cycle –
amplitude is symmetrical about the
mean zero stress level. Typical of
laboratory testing and may be
experienced by a rotating shaft
operating at constant speed
(without overloads)
2.Repeated stress cycle – amplitude
is asymmetrical about the mean
zero stress level. In this case σmax
is tension and σmin is compression,
but both could be tension.
3. Random (or spectrum) stress
cycle, such as may be
experienced by an aircraft wing
or an automotive suspension
component etc. Unexpected
overloads may occur due to
(say) turbulence or bumpy road
conditions.
How does high cycle fatigue(HCF) and low cycle fatigue(LCF) affect and vary?
Low-Amplitude Vibration (Acoustic)
Effect: Elastic response (e.g., ringing a bell)
Result: No permanent damage
Curve: Labelled ‘a’
2. Increased Amplitude Vibration
Effect: Permanent damage begins (fatigue)
Cause: Cyclic stress → Dislocation activity → Crack formation
Result: Crack propagates until reaching a critical size for fracture
3. Low-Cycle Fatigue (Curve ‘c’)
Condition: Stress cycles above the yield strength of the material
Effect: Failure occurs after few cycles
Result: Plastic deformation and failure
4. High-Cycle Fatigue (Curve ‘b’)
Condition: Stresses below the yield strength
Effect: Elastic stress, but plastic deformation may occur at the crack tip
Result: Failure after many cycles
How is fatigue failure usually modelled / plotted?
It is plotted on a stress amplitude against log number of cycles to failure known as an S-N curve.
What is the fatigue limit?
Known as the endurance limit. The stress amplitude about a zero mean stress below which fatigue failure will never occur. e.g in steel or titanium alloys
Non-ferrous alloys do not exhibit this limit as fatigue can occur regardless therefore ‘fatigue strength’ is used here after N cycles
What is the fatigue life?
Number of cycles to failure at a specified stress amplitude
What does the fracture toughness describe?
The critical stress for the propagation of a sharp crack of a certain size so = critical stress intensity factor. It measures the resistance to brittle fracture when a crack is present. KI is larger for touch materials and low for brittle materials.
How does the plastic zone relate to the yield strength?
As the yield strength increases from material shrinkage. A crack in soft metal will have a large plastic zone whereas a ceramic or glass with a high yield strength will have a small plastic zone.
What is stress corrosion cracking(SCC)?
Refers to cracking due to the
simultaneous action of a (specific) corrosion environment under an applied and/or residual tensile stress. Can lead to a significant reduction in the material strength with minimal material loss. Damage is largely hidden and can result in fast and catastrophic final failure.
Sometimes described as a subset of phenomena of embrittlement including hydrogen embrittlement / anodic dissolution