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Component failure in road traffic accident by ayoub el amri

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Component Failure in road trafic accidents By : AYOUB EL AMRI. 1
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Page 1: Component failure in road traffic accident by ayoub el amri

Component Failure in road trafic accidents

By : AYOUB EL AMRI.

1

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How do Materials Break?

Chapter Outline: Failure

Ductile vs. brittle fracture

Principles of fracture mechanics

Stress concentration

Impact fracture testing

Fatigue (cyclic stresses)

Cyclic stresses.

Crack initiation and propagation

Factors that affect fatigue behavior

Creep (time dependent deformation)

Stress and temperature effects

Alloys for high-temperature use

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Brittle vs. Ductile Fracture

• Ductile materials - extensive plastic deformation

and energy absorption (“toughness”) before

fracture

• Brittle materials - little plastic deformation and

low energy absorption before fracture

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Brittle vs. Ductile Fracture

A. Very ductile: soft metals (e.g. Pb, Au) at

room T, polymers, glasses at high T

B. Moderately ductile fracturetypical for metals

C. Brittle fracture: ceramics, cold metals,

A B C

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Steps : crack formation

crack propagation

Fracture

Ductile vs. brittle fracture

• Ductile - most metals (not too cold):

Extensive plastic deformation before

crack

Crack resists extension unless applied

stress is increased

• Brittle fracture - ceramics, ice, cold

metals:

Little plastic deformation

Crack propagates rapidly without

increase in applied stress

Ductile fracture is preferred in most applications

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Ductile Fracture (Dislocation Mediated)

(a) Necking, (b) Cavity Formation,

(c) Cavities coalesce form crack

(d) Crack propagation, (e) Fracture

Crack

grows

90o to

applied

stress

45O -

maximum

shear

stress

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Ductile Fracture

(Cup-and-cone fracture in Al)

Scanning Electron Microscopy. Spherical

“dimples” micro-cavities that initiate crack

formation.

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Crack propagation is fast

Propagates nearly perpendicular to

direction of applied stress

Often propagates by cleavage -

breaking of atomic bonds along specific

crystallographic planes

No appreciable plastic deformation

Brittle Fracture (Low Dislocation Mobility)

Brittle fracture in a mild steel

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A. Transgranular fracture: Cracks pass through

grains. Fracture surface: faceted texture because of

different orientation of cleavage planes in grains.

B. Intergranular fracture: Crack propagation is

along grain boundaries (grain boundaries are

weakened/ embrittled by impurity segregation etc.)

A B

Brittle Fracture

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Fracture strength of a brittle solid:

related to cohesive forces between atoms.

Theoretical strength: ~E/10

Experimental strength ~ E/100 - E/10,000

Difference due to:

Stress concentration at microscopic flaws

Stress amplified at tips of micro-cracks etc.,

called stress raisers

Stress Concentration

Figure by

N. Bernstein &

D. Hess, NRL

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Stress Concentration

0 = applied stress; a = half-length of crack;

t = radius of curvature of crack tip.

Stress concentration factor

2/1

t

0m

a2

Crack perpendicular to applied stress:

maximum stress near crack tip

2/1

t0

mt

a2K

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Two standard tests: Charpy and Izod. Measure the

impact energy (energy required to fracture a test piece

under an impact load), also called the notch toughness.

Impact Fracture Testing

CharpyIzod

h’

h

Energy ~ h - h’

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As temperature decreases a ductile

material can become brittle

Ductile-to-Brittle Transition

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Low temperatures can severely embrittle steels. The

Liberty ships, produced in great numbers during the WWII

were the first all-welded ships. A significant number of

ships failed by catastrophic fracture. Fatigue cracks

nucleated at the corners of square hatches and propagated

rapidly by brittle fracture.

Ductile-to-brittle transition

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Under fluctuating / cyclic stresses,

failure can occur at lower loads than

under a static load.

90% of all failures of metallic

structures (bridges, aircraft, machine

components, etc.)

Fatigue failure is brittle-like –

even in normally ductile materials.

Thus sudden and catastrophic!

Fatigue

Failure under fluctuating stress

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Fatigue: Cyclic StressesCharacterized by maximum, minimum and mean

Range of stress, stress amplitude, and stress ratio

Mean stress m = (max + min) / 2

Range of stress r = (max - min)

Stress amplitude a = r/2 = (max - min) / 2

Stress ratio R = min / max

Convention: tensile stresses positive

compressive stresses negative

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Fatigue: Crack initiation+ propagation (I)

Three stages:

1. crack initiation in the areas of stress

concentration (near stress raisers)

2. incremental crack propagation

3. rapid crack propagation after crack

reaches critical size

The total number of cycles to failure is the sum of cycles

at the first and the second stages:

Nf = Ni + Np

Nf : Number of cycles to failure

Ni : Number of cycles for crack initiation

Np : Number of cycles for crack propagation

High cycle fatigue (low loads): Ni is relatively high.

With increasing stress level, Ni decreases and Np

dominates

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Fatigue: Crack initiation and propagation (II)

Crack initiation: Quality of surface and sites

of stress concentration

(microcracks, scratches, indents, interior

corners, dislocation slip steps, etc.).

Crack propagation

I: Slow propagation along

crystal planes with high

resolved shear stress.

Involves a few grains.

Flat fracture surface

II: Fast propagation

perpendicular to applied

stress.

Crack grows by repetitive

blunting and sharpening

process at crack tip.

Rough fracture surface.

Crack eventually reaches critical dimension and

propagates very rapidly

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Factors that affect fatigue life

Magnitude of stress

Quality of the surface

Solutions:

Polish surface

Introduce compressive stresses (compensate for

applied tensile stresses) into surface layer.

Shot Peening -- fire small shot into surface

High-tech - ion implantation, laser peening.

Case Hardening: Steel - create C- or N- rich

outer layer by atomic diffusion from surface

Harder outer layer introduces compressive

stresses

Optimize geometry

Avoid internal corners, notches etc.

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Factors affecting fatigue life

Environmental effects

Thermal Fatigue. Thermal cycling causes

expansion and contraction, hence thermal stress.

Solutions:

change design!

use materials with low thermal expansion

coefficients

Corrosion fatigue. Chemical reactions induce

pits which act as stress raisers. Corrosion also

enhances crack propagation.

Solutions:

decrease corrosiveness of medium

add protective surface coating

add residual compressive stresses

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Creep

Creep testing

Furnace

Time-dependent deformation due to

constant load at high temperature

(> 0.4 Tm)Examples: turbine blades, steam generators.

Creep test:

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Stages of creep

1. Instantaneous deformation, mainly elastic.

2. Primary/transient creep. Slope of strain vs.

time decreases with time: work-hardening

3. Secondary/steady-state creep. Rate of straining

constant: work-hardening and recovery.

4. Tertiary. Rapidly accelerating strain rate up to

failure: formation of internal cracks, voids,

grain boundary separation, necking, etc.

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Parameters of creep behavior

Secondary/steady-state creep:

Longest duration

Long-life applications

Time to rupture ( rupture lifetime, tr):

Important for short-life creep

t/s

tr

/t

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Creep: stress and temperature effects

With increasing stress or temperature:

The instantaneous strain increases

The steady-state creep rate increases

The time to rupture decreases

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Creep: stress and temperature effects

Stress/temperature dependence of the steady-state

creep rate can be described by

RT

QexpK cn

2s

Qc = activation energy for creep

K2 and n are material constants

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Alloys for High-Temperatures(turbines in jet engines, hypersonic

airplanes, nuclear reactors, etc.)

Creep minimized in materials with

High melting temperature

High elastic modulus

Large grain sizes

(inhibits grain boundary sliding)

Following materials (Chap.12) are especially

resilient to creep:

Stainless steels

Refractory metals (containing elements of

high melting point, like Nb, Mo, W, Ta)

“Superalloys” (Co, Ni based: solid solution

hardening and secondary phases)

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Summary

Brittle fracture

Charpy test

Corrosion fatigue

Creep

Ductile fracture

Ductile-to-brittle transition

Fatigue

Fatigue life

Fatigue limit

Fatigue strength

Impact energy

Intergranular fracture

Stress raiser

Thermal fatigue

Transgranular fracture

Make sure you understand language and concepts:

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Thank you for your attention.

Any questions?


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