ISSUES TO ADDRESS...
• How do flaws in a material initiate failure?
• How is fracture resistance quantified; how do different material classes compare?
• How do we estimate the stress to fracture?
• How do loading rate, loading history, and temperature affect the failure stress?
Ship-cyclic loading from waves.
Computer chip-cyclic thermal loading.
Hip implant-cyclic loading from walking.
1

• Ductile failure:
--one piece
--large deformation
• Brittle failure:
--many pieces
--small deformation
3

• Evolution to failure: necking
 void nucleation void growth and linkage shearing at surface fracture
• Resulting fracture surfaces
(steel) particles serve as void nucleation sites.
50 m m m
100 m m
4

• Inter granular
( between grains) 304 S. Steel
(metal)
• Intra granular
( within grains)
316 S. Steel
(metal)
4 mm
Polypropylene
(polymer)
Al Oxide
(ceramic)
160 m m
1 mm
3 m m
5

• Stress-strain behavior (Room T): materials perfect materials
• DaVinci (500 yrs ago!) observed...
--the longer the wire, the smaller the load to fail it.
• Reasons:
--flaws cause premature failure.
--Larger samples are more flawed!
6

• Elliptical hole in • Stress distrib. in front of a hole: a plate:
• Stress conc. factor:
• Large K t promotes failure:
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2.5
Stress Conc. Factor, K t
=
 max
 o
2.0
increasing w/h
1.5
1.0
0 0.5
1.0
sharper fillet radius r/h
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• r t at a crack tip is very small!
• Result: crack tip stress is very large.
 tip
• Crack propagates when: the tip stress is large enough to make:
K ≥ K c
 tip

K
2  x increasing K distance, x , from crack tip
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• Condition for crack propagation:
K ≥ K c
Stress Intensity Factor :
--Depends on load & geometry.
Fracture Toughness:
--Depends on the material, temperature, environment, & rate of loading.
• Values of K for some standard loads & geometries:
 units of K :
MPa m or ksi in
K
   a K

1.1
  a
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FRACTURE TOUGHNESS
Based on data in Table B5,
Callister 6e .
Composite reinforcement geometry is: f = fibers; sf = short fibers; w = whiskers; p = particles. Addition data as noted (vol. fraction of reinforcement):
1. (55vol%) ASM Handbook , Vol. 21, ASM
Int., Materials Park, OH (2001) p. 606.
2. (55 vol%) Courtesy J. Cornie, MMC, Inc.,
Waltham, MA.
3. (30 vol%) P.F. Becher et al., Fracture
Mechanics of Ceramics , Vol. 7, Plenum
Press (1986). pp. 61-73.
4. Courtesy CoorsTek, Golden, CO.
5. (30 vol%) S.T. Buljan et al., "Development of Ceramic Matrix Composites for
Application in Technology for Advanced
Engines Program", ORNL/Sub/85-22011/2,
ORNL, 1992.
6. (20vol%) F.D. Gace et al., Ceram. Eng.
Sci. Proc.
, Vol. 7 (1986) pp. 978-82.
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DESIGN AGAINST CRACK GROWTH
• Crack growth condition: K ≥ K c
Y
  a
• Largest , most stressed cracks grow first!
--Result 1: Max flaw size dictates design stress.
 design

K c
Y
 a max
--Result 2: Design stress dictates max. flaw size.
a max

1



Y

K c design


2
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• Material has K c
= 26 MPa-m 0.5
• Two designs to consider...
Design A Design B
--largest flaw is 9 mm --use same material
--failure stress = 112 MPa --largest flaw is 4 mm
 c
K c
--failure stress = ?
• Use...

Y
 a max
• Key point: Y and K c are the same in both designs.
--Result:
112 MPa 9 mm 4 mm

 c a max

A
 c a max

B
Answer:
 
B

168MPa
• Reducing flaw size pays off!
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• Increased loading rate...
--increases  y and TS
--decreases %EL
• Why?
An increased rate gives less time for disl. to move past obstacles.
• Impact loading:
--severe testing case
--more brittle
--smaller toughness sample final height initial height
14

• Increasing temperature...
--increases %EL and K c
• Ductile-to-brittle transition temperature (DBTT) ...
15

• Pre-WWII: The Titanic • WWII: Liberty ships
• Problem: Used a type of steel with a DBTT ~ Room temp.
16

• Engineering materials don't reach theoretical strength .
• Flaws produce stress concentrations that cause premature failure.
• Sharp corners produce large stress concentrations and premature failure.
• Failure type depends on T and stress:
for noncyclic  and T < 0.4T
m
, failure stress decreases with: increased maximum flaw size, decreased T, increased rate of loading.
-for cyclic  : cycles to fail decreases as D increases.
-for higher T (T > 0.4T
m
): time to fail decreases as  or T increases.
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