Chapter 8 mechanical failure
-
Upload
meelu-qazi -
Category
Technology
-
view
4.140 -
download
1
Transcript of Chapter 8 mechanical failure
![Page 1: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/1.jpg)
MSE-211-Engineering Materials 1
Mechanical Failure
Chapter reading 8 ISSUES TO ADDRESS...
1
• How do cracks that lead to failure form?
• How is fracture resistance quantified? How do the fracture
resistances of the different material classes compare?
• How do we estimate the stress to fracture?
• How do loading rate, loading history, and temperature
affect the failure behavior of materials?
Ship-cyclic loading
from waves.
Computer chip-cyclic
thermal loading.
Hip implant-cyclic
loading from walking.
![Page 2: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/2.jpg)
MSE-211-Engineering Materials 2
Mechanical Failure
Why study failure?
Design of a component or structure: Minimize failure possibility
It can be accomplished by understanding the mechanics of failure
modes and applying appropriate design principles.
Failure cost
1. Human life 2. Economic loss 3.Unavailability of service
Failure causes:
1. Improper material selection 2. Inadequate design 3. Processing
Regular inspection, repair and replacement critical to safe design
![Page 3: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/3.jpg)
MSE-211-Engineering Materials 3
Fracture
Fracture is the separation of a body into two or more
pieces in response to an imposed stress
Steps in Fracture:
Crack formation
Crack propagation
![Page 4: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/4.jpg)
MSE-211-Engineering Materials 4
Fracture Modes
Depending on the ability of material to undergo plastic deformation
before the fracture two fracture modes can be defined - ductile or
brittle.
Ductile fracture - most metals (not too cold):
Extensive plastic deformation ahead of crack
Crack is “stable”: resists further extension
unless applied stress is increased
Brittle fracture - ceramics, ice, cold metals:
Relatively little plastic deformation
Crack is “unstable”: propagates rapidly without
increase in applied stress
Ductile fracture is preferred in most applications
![Page 5: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/5.jpg)
MSE-211-Engineering Materials 5
Ductile Vs Brittle Fracture
Very
Ductile
Moderately
Ductile Brittle
Fracture
behavior:
Large Moderate %AR or %EL Small
![Page 6: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/6.jpg)
MSE-211-Engineering Materials 6
Ductile Fracture
• Evolution to failure:
(a) (b) (c) (d) (e)
(a) Necking
(b) Formation of microvoids
(c) Coalescence of microvoids to form a crack
(d) Crack propagation by shear deformation
(e) Fracture
Cup and cone
fracture
![Page 7: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/7.jpg)
MSE-211-Engineering Materials 7
(Cup-and-cone fracture in Al)
Ductile Vs Brittle Fracture
brittle fracture ductile fracture
Brittle fracture in a mild steel
![Page 8: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/8.jpg)
MSE-211-Engineering Materials
Ductile Fracture
(a) SEM image showing spherical dimples resulting from a
uniaxial tensile load representing microvoids. (b) SEM image of
parabolic dimples from shear loading.
8
![Page 9: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/9.jpg)
MSE-211-Engineering Materials 9
Brittle Fracture
Arrows indicate point at failure origination
Distinctive pattern on the fracture surface: V-shaped “chevron”
markings point to the failure origin.
![Page 10: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/10.jpg)
MSE-211-Engineering Materials 10
Brittle Fracture
Lines or ridges that radiate from the origin of
the crack in a fanlike pattern
![Page 11: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/11.jpg)
MSE-211-Engineering Materials 11
Transgranular fracture
Fracture cracks pass through grains.
![Page 12: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/12.jpg)
MSE-211-Engineering Materials 12
Intergranular fracture: Fracture crack propagation is
along grain boundaries (grain boundaries are weakened
or embrittled by impurities segregation etc.)
![Page 13: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/13.jpg)
MSE-211-Engineering Materials 13 13 13
• Ductile failure:
-- one piece
-- large deformation
Example: Pipe Failures
• Brittle failure:
-- many pieces
-- small deformations
![Page 14: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/14.jpg)
MSE-211-Engineering Materials 14
Studies the relationships between:
material properties
stress level
crack producing flaws
crack propagation mechanisms
Fracture Mechanics
![Page 15: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/15.jpg)
MSE-211-Engineering Materials 15
Stress Concentration
Measured fracture strength is much lower than predicted by calculations
based on atomic bond energies. This discrepancy is explained by the
presence of flaws or cracks in the materials.
The flaws act as stress concentrators or stress raisers,
amplifying the stress at a given point.
The magnitude of amplification depends on crack
geometry and orientation.
![Page 16: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/16.jpg)
MSE-211-Engineering Materials 16
Stress Concentration
![Page 17: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/17.jpg)
MSE-211-Engineering Materials 17
Stress Concentration
If the crack is similar to an elliptical
hole through plate, and is oriented
perpendicular to applied stress, the
maximum stress, at crack tip
where t = radius of curvature
so = applied stress
sm = stress at crack tip
a = length of surface crack or ½
length of internal crack
2/1
2
t
om
a
ss
![Page 18: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/18.jpg)
MSE-211-Engineering Materials 18
Stress Concentration
2/1
2
t
om
a
ss
The stress concentration factor is
A measure of the degree to which an external
stress is amplified at the tip of a crack.
(1)
Rearranging equation 1
sm 2so
a
t
1/2
Ktso
![Page 19: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/19.jpg)
MSE-211-Engineering Materials 19 19
Engineering Fracture Design
r/h
sharper fillet radius
increasing w/h
0 0.5 1.0 1.0
1.5
2.0
2.5
Stress Conc. Factor, K t =
• Avoid sharp corners! s
Adapted from Fig.
8.2W(c), Callister 6e.
(Fig. 8.2W(c) is from G.H.
Neugebauer, Prod. Eng.
(NY), Vol. 14, pp. 82-87
1943.)
r , fillet
radius
w
h
smax
smax
s0
![Page 20: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/20.jpg)
MSE-211-Engineering Materials 20
Stress Concentration
Crack propagation
Cracks with sharp tips propagate easier than cracks having blunt tips
2/1
2
t
om
a
ss
In ductile materials, plastic deformation at a crack tip “blunts” the crack.
![Page 21: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/21.jpg)
MSE-211-Engineering Materials 21
Crack propagation
Stress Concentration
Critical stress for crack propagation
γs = specific surface energy
When the tensile stress at the tip of crack exceeds the critical stress value
the crack propagates and results in fracture.
![Page 22: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/22.jpg)
MSE-211-Engineering Materials 22
EXAMPLE PROBLEM 8.1 Page 244
A relatively large plate of a glass is subjected to a tensile stress of 40
MPa. If the specific surface energy and modulus of elasticity for this
glass are 0.3 J/m2 and 69 GPa, respectively, determine the maximum
length of a surface flaw that is possible without fracture.
𝑎 =2𝐸𝛾𝑠
𝜋𝜎2
𝐸 = 69 𝐺𝑃𝑎
𝛾𝑠 =0.3 J/m2
𝜎 = 40 𝑀𝑃𝑎
Rearranging the equation
𝑎 = 8.2 * 10-6 m
![Page 23: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/23.jpg)
MSE-211-Engineering Materials 23
Home Work Problems
Exercise Problems 8.1-8.4
![Page 24: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/24.jpg)
MSE-211-Engineering Materials 24
Fracture Toughness
• Fracture toughness measures a material’s resistance to
fracture when a crack is present.
• It is an indication of the amount of stress required to propagate a preexisting flaw.
𝐾𝑐 = 𝜎𝑐 𝜋𝑎
𝐾𝑐= Fracture toughness
![Page 25: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/25.jpg)
MSE-211-Engineering Materials 25
Fracture Toughness
𝑲𝒄is a material property depends on temperature, strain rate
and microstructure.
The magnitude of Kc diminishes with increasing strain rate
and decreasing temperature.
Improvement in yield strength wrought by alloying and
strain hardening generally produces corresponding decrease
in Kc .
Kc normally increases with reduction in grain size as
composition and other microstructural variables are
maintained constant.
![Page 26: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/26.jpg)
MSE-211-Engineering Materials 26
Impact Fracture Testing
Testing fracture characteristics under high strain rates
Two standard tests, the Charpy and Izod, measure the impact
energy (the energy required to fracture a test piece under an
impact load), also called the notch toughness
![Page 27: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/27.jpg)
MSE-211-Engineering Materials 27
(Charpy)
Impact Fracture Testing
Izod
final height initial height
![Page 28: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/28.jpg)
MSE-211-Engineering Materials 28
Ductile-to- brittle transition
As temperature decreases a ductile material can become
brittle - ductile-to-brittle transition.
The ductile-to-brittle transition can be measured by impact testing:
the impact energy needed for fracture drops suddenly over a
relatively narrow temperature range – temperature of the ductile-to-
brittle transition.
The ductile to-brittle transition is related to the temperature
dependence of the measured impact energy absorption
![Page 29: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/29.jpg)
MSE-211-Engineering Materials 29 29
Adapted from Fig. 8.15,
Callister & Rethwisch 8e.
• Ductile-to-Brittle Transition Temperature (DBTT)...
Low strength steels(BCC)
Imp
act E
ne
rgy
Temperature
High strength materials
polymers
More Ductile Brittle
Ductile-to-brittle transition temperature
Low strength (FCC and HCP) metals (e.g., Cu, Ni)
![Page 30: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/30.jpg)
MSE-211-Engineering Materials 30
• Pre-WWII: The Titanic • WWII: Liberty ships
• Problem: Steels were used having DBTT’s just below
room temperature.
Design Strategy:
Stay Above The DBTT!
![Page 31: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/31.jpg)
MSE-211-Engineering Materials 31
Fatigue
Failure under fluctuating / cyclic stresses
e.g., bridges, aircraft, machine components, automobiles,etc..
Fatigue
• Stress varies with time.
s max
s min
s
time
s m S
![Page 32: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/32.jpg)
MSE-211-Engineering Materials 32
Fatigue failure can occur at loads considerably lower
than tensile or yield strengths of material under a static
load.
Fatigue
Estimated to causes 90% of all failures of metallic structures
Fatigue failure is brittle-like (relatively little plastic
deformation) - even in normally ductile materials. Thus
sudden and catastrophic!
Fatigue failure proceeds in three distinct stages: crack
initiation in the areas of stress concentration (near stress
raisers), incremental crack propagation, final catastrophic
failure.
![Page 33: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/33.jpg)
MSE-211-Engineering Materials 33
Fatigue
CYCLIC STRESSES
1.Reversed stress cycle
Periodic and symmetrical
about zero stress
2.Rpeated stress cycle
Periodic and asymmetrical
about zero stress
![Page 34: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/34.jpg)
MSE-211-Engineering Materials 34
Fatigue
CYCLIC STRESSES
3.Random stress cycle Random stress fluctuations
![Page 35: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/35.jpg)
MSE-211-Engineering Materials 35
Fatigue
CYCLIC STRESSES
Mean stress (𝜎𝑚)
![Page 36: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/36.jpg)
MSE-211-Engineering Materials 36
![Page 37: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/37.jpg)
MSE-211-Engineering Materials 37
Fatigue
S — N curves
(stress — number of cycles to failure)
Fatigue properties of a material (S-N curves) are tested in
rotating-bending tests in fatigue testing apparatus
Result is commonly plotted as S (stress) vs. N (number of
cycles to failure)
![Page 38: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/38.jpg)
MSE-211-Engineering Materials 38
S — N curves
Fatigue limit (endurance limit) occurs for some materials
(e.g. some Fe and Ti alloys). In this case, the S—N curve
becomes horizontal at large N, limiting stress level. The fatigue
limit is a maximum stress amplitude below which the material
never fails, no matter how large the number of cycles is.
For many steels,
fatigue limits
range between
35% and 60%
of the tensile
strength.
![Page 39: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/39.jpg)
MSE-211-Engineering Materials 39
S — N curves
In most non ferrous alloys(e.g., Aluminum, Copper,
Magnesium) S decreases continuously with N. In this
cases the fatigue properties are described by
Fatigue strength: stress at which
fracture occurs after a
specified number of cycles (e.g.
107)
Fatigue life: Number of cycles to
fail at a specified stress
level
![Page 40: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/40.jpg)
MSE-211-Engineering Materials 40
![Page 41: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/41.jpg)
MSE-211-Engineering Materials 41
Fatigue
Fracture surface characteristics
Beach marks and striations
![Page 42: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/42.jpg)
MSE-211-Engineering Materials 42
Creep is a time-dependent and permanent deformation
of materials when subjected to a constant load or stress.
For metals it becomes important at a high temperature
(> 0.4 Tm). Examples: turbine blades, steam
generators, high pressure steam lines.
Creep
Polymers are specially sensitive to creep.
For details read the book pages 265-267
![Page 43: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/43.jpg)
MSE-211-Engineering Materials 43
Stages of Creep
![Page 44: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/44.jpg)
MSE-211-Engineering Materials 44
1. Instantaneous deformation, mainly elastic.
2. Primary/transient creep. Slope of strain vs. time
decreases with time: strain-hardening
3. Secondary/steady-state creep. Rate of straining is
Constant
4. Tertiary. Rapidly accelerating strain rate up to
failure:
formation of internal cracks, voids, grain boundary
separation, necking, etc.
Stages of Creep
![Page 45: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/45.jpg)
MSE-211-Engineering Materials 45
Parameters of creep behavior
The stage of secondary/steady-state creep is of longest
duration and the steady-state creep rate 𝜺.𝒔 =
∆𝜺
∆𝒕.is the
most important parameter of the creep behavior in long-life
applications e.g. nuclear power plant component.
Another parameter, especially important in short-life
creep situations, is time to rupture, or the rupture
lifetime, tr.. e.g., turbine blades in military aircraft and
rocket motor nozzles, etc….
![Page 46: Chapter 8 mechanical failure](https://reader034.fdocuments.us/reader034/viewer/2022042504/554a4639b4c905863d8b540a/html5/thumbnails/46.jpg)
MSE-211-Engineering Materials 46
Creep: stress and temperature effects