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7/27/2019 1 Plastic Deformation 2013 (1)
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1: Plastic deformation
Stefan Jonsson
2013
Technological and true definitions
Le
ln
L
L
L
dLL
LdL
d
0A
Ps
0
A
P
L0 + L = L
P P
A0
A
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Elastic and plastic volumechange
000 LA
P P zzyyxxel
V
V
0
000 LAALV
Volume is unaffected by plastic deformation
because no atoms are added/removed.
True & technological relations
0 LLLL
000 LLL
)1(0
0
0000esL
LLsLA
LP
LAA
ALP
A
P
e
s
.
variables with the wanted ones.
Remember V = constant
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True and technological curves
400
450
150
200
250
300
350
s
,,
[MPa]
true valuesSSAB, Tunnplt
es
< e
> s
0
50
100
0 2 4 6 8 10 12 14 16 18 20 22
e , , [%]
tech valuesDomex DD 200, Rolling directionstrain rate: 5E-03 (1/s)
Addition of strains
toteLLLL
eee
0
03
2
23
1
12
0
01321
tot
L
L
L
L
L
L
L
LL
dL
L
dL
L
dL
L
dL
3
0
3
2
2
1
1
0
321
Only true strains can be added linearly
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Elastic and plastic deformation
petot
pe
y
y
p e
Elastic and plastic deformation
y
Elastic deformation,
full recoverable
Elastic & plastic
deformation,
partly recoverable
p eAs long as there is a stress,
there is an elastic deformation!
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Necking
P2 P2
P1 P1
A B t0
t1
t2
xy
z
m03:i
n
A
B
t1 t2
1
t0
Deformation is
homogeneous until
onset of necking
y
1
n
A
B
t1
t2
t0
When a neck is
formed, deformation
becomes highly
localized
Instability criterion for straining
ddAdA
ddAddA
dAdA
dP
P=[(y)]A[(y)] V=A()L() ?
dydddyddyddydydy
0
AddA
Ld
dL
Ad
dA
Ld
dL
Ad
dA
Ld
dV
AdA
For homogeneous
0
dy
dA
d
d
dy
dP
0
dy
d0
d
d
Hom. Deform. Necking
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Macro- & microscopic deform.
P P
deformation
is only an
average over
the sample
volume.
Much
information is
hidden.
The Bauschinger effect
soft
, ||
f
b
easier
permanent softening
f
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Definitions
o po n s
on the
stress
s
Yield stressProportionality
(Ultimate)
Tensile strength
curvee
0.2%homogeneousdeformation
necking fracture
Lders strain
Propagating y
er s an s
Inhomogeneous
deformation Upper & lower
yield stress
u
L
Continues with
normal plastic
deformationL
l
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Strain rate sensitivity
)( fm
logln
m
)(logloglog fm
ogn Increasedstrain rate
Elongation v.s. m-value
011
md
m
f
/
)(
1
Deformation
continues outside
the neck
Grain boundary
sliding gives high
m-values
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Superplasticity
Grain boundary sliding
Limited to a range in T and strain rate
Total strain energy
ddLPdLPdW
200
250
300
350
400
450
,
[MPa]
2
1
dWV
0
50
100
150
0 5 10 15 20
, [%]
Per volume unit!!
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Elastic strain energy
Eheigthwidth
W elV
2
250
300
350
400
450
,[MPa]
0
50
100
150
0 5 10 15 20
, [%]
Plastic strain energy
400
450
400
450
0
50
100
150
200
250
300
350
0 5 10 15 20
, [%]
,
[MPa]
0
50
100
150
200
250
300
350
0 5 10 15 20
, [%]
,
[MPa]
pl
V
pl
V
el
V
tot
V WWWW
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Forcesonabody
2
3Face 3
1
Face 2
Face 1
F
FN
F
F2
T
F = FT + FN = F1 + F2 + F3
Forcesoneach surface produces 1normalstress
and2perpendicular shear stresses
Stress components
2
333
333231
232221
131211
ij
1
11
22
Firstindex: Forcedirection
Secondindex: Faceindex
33
2322
131211
ij
ij = ji32 32
23
23Symm.
6independentelementsofthestresstensor
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Normalstrains,iiMechanical equilibrium,i.e.no
accelerationsarecreated by
11
3
11
22
applied stresses.
11
22 2233
1 2
33
03322110
VV
33
0332211
Normalplasticstrain shall not
produce volume change.
Positiveshear stress;12=21
2
3
12-plane
Neutral direction
1
Mechanical equilibrium,i.e.no
rotationsarecreated byapplied
shear stresspairShear deformationcannot
produce volume change.
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Negativeshear stress;12=21
2
3
12-plane
Neutral direction
1
Positiveshear stress;13=31
2
3Neutral direction
1
13-plane
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Negativeshear stress;13=31
2
3Neutral direction
1
13-plane
Positiveshear stress;23=32
2
3
Neutral direction
1
23-plane
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Negativeshear stress;23=32
2
3
Neutral direction
1
23-plane
Shear strains;ij=ji
1 2
3
NOTE!ij=ji
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Definitionofstrain tensorDisplacements u1,u2andu3are
found bymoving inx1,x2andx3
i
j
j
iij
x
u
x
u
2
1
Thetensor comp.isacombination
oftwo dis lacements u andu
Thetensor comp.isthe
displacement,uifound
bymoving inxi
i=j
i
1 2
3
found bymoving inxjandxi
ji
j
i
i
j
i
j
j
iij
x
u
x
u
x
u
x
u
2
1
2
1
Engineering shear, y
Pure shear ySimple shear
x2
1
x
1
Produced bydislocation slip
21 jiijij
ijjiiji
j
j
iij
x
u
x
u
2
1
2
1
2
1
This is only half of the
engineering shear!!
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Strain components, ij
0
02
1
00
00
3231
2321
33
22
332313
232212
ij
5 Independent strains: 2 3
Symm. Symm. Symm.
AngularVolumetric
03322110
VV
5 independent slip systems must be activated to produce a general deformation.
Fragmentation of grains reduces this number locally.
e orma one orma on
Stress states
y
x
h
tanh
cos
yy
xx
xy
xy
2cos2sin2
cossin2sincos 22
xy
xxyy
xyyyxx
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Mohrs circle for stresses (xx ,xy)
R (, )
(1 ,0)(2 ,0)
( ,-x )
22
2sinxy
R
R
R
yyxx
yyxx
)(2
1
)(2
1
2
1
2
2
2
22cos
xy
yyxx
yyxx
R
R
Rotationbetween principaldirections
z
z
=90 =45 0
y
y
z
y
2=180 2=90 20
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45 direction isbestforone principal
stress
zz zz zz
=45
zz zz zz
2=90
2
zz
General stress state
31
123
z
zz
yyxx
yzzy
zx
yx xy
xz
2max
x
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123
Hydrostatic
pressure
hydrostatic
pressure
123
Tri-axial stress state
)(2
131max
3
123
1
2
3
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Spherical stress state
3=2=1
Cylindrical stress state
13=2
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Planar stress state
13= 2Free surface
Membranes
12=3
23
1=
Slipsystemsinfcc
110111typeofsSlipsystem12
110typeofvectorsBurgers3
111typeofslipplanes4
0bn
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Slipsystemsinbcc
110typeofslipplanes6 112typeofslipplanes12
111110typeofsSlipsystem12 ypeovec orsurgers
111112typeofsSlipsystem12ypeovec orsurgers
Totally 24 slip systems are easily activated.
Critically resolved shear stresses, CRSS, are
different for {110} and {112}
SlipsystemsinhcpEasily
activated
0211(0001)typeofsSlipsystem3
0211typeofvectorsBurgers3
0001(slipplanebasal1 )
02110011typeofsSlipsystem3
0211typeofvectorsBurgers1
0011slipplanesprismatic3
6 easily activated slip systems, different CRSS
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Schmids formula,CRSS,c
0P0P
cos0PPb
b1
b2
b3
cos0A
coscos
cos/
cos
0
0
A
Pgb
dA=ab/cos
=dA0cos
a/cos
cos0PPn
c coscos
A0a b
dA0=ab
Taylors formula (inverted Schmid)
c coscos dddW
cy Single
cc m
coscos
1
cy m
m
ddd
y
c
m
Averaging
Pol cr stals
06.3
06.3
8.2
hcp
fcc
bcc
m
m
mRandom
orientations
bcc deforms best
hcp deforms worst