finite element analysis of central bursting defects occurring in...
TRANSCRIPT
Finite element analysis of central bursting defects
occurring in cold forward extrusion
1) Graduate student of Gyeongsang National University(GNU), Jinju / Korea; 2) Korea Institute of Industrial Technology, Incheon / Korea; 3) Youngsin Metal Industrial Co., Ltd. Pyeongtaek / Korea; #) School of Mechanical and Areospace Engineering, GNU, Jinju / Korea, [email protected]
MSEC2011, June 14, 2011
MS Joun #), MC Kim 1), DJ Yoon2) , HJ Choi2), YH Son3)
www.afdex.com
AFDEX
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Contents
⊙ Research background
⊙ Examples of central bursting defects
and finite element predictions
⊙ Application of finite element analysis to tensile test
⊙ Scheme of analyzing crack propagation
⊙ Finite element analysis of fracture phenomena in tensile test
⊙ Finite element analysis of the central bursting defects
⊙ Conclusions
Research background – Forging defects
Hot shortness
Metal flow Buckling
Shape defect
Folding
Under-filling
Air-trapping
Piping
Ductile fracture
Bad spheroidizing
Chevron crack
Research background
⊙ Chevron defect has been well known and found at times
⊙ Chevron defects may lead to big accidents.
⊙ High strength-low strain hardening material is exposed to chevron defects.
⊙ Survey of the literature
○ Jennison, design parameters
○ Avizur, relatively small load/ Coulomb friction, die angle and reduction area
○ Kachanov, crack generation criterion
○ Soyarslan, et al., micro-voids, macro-crack
○ McAllen, et al., safe reduction ratios below 7%/ die land effect
○ Many researches have obtained finite element predictions of chevron crack
propagation, but most research works are different from actual experiments.
Previous studies on central bursting defects
C. Soyarslan et al.
ABAQUS/ Explicit
Elasto-plastic
K. Saanouni et al.
Forge
Elasto-plastic
H. Cho et al.
DEFORM
Labergeere et al.
ABAQUS/ Explicit
thermoelasto-viscoplastic
F. Ahmadi et al.
Rigid-plastic
McAllen et al.
ABAQUS
EXPERIMENTS
PREDICTIONS
Extrusion Drawing
cr
or100c
o
rr
r
81r
90r 78r 84r
72r 38r 67r 55r 60.0r 50r
83meanr
Previous studies on material identification
⊙ K. Komori, 2002, Simulation of tensile test by node separation method.
○ Axi-symmetric, Rigid-plastic.
○ Fracture load
1 2
(1 ) (1)
(1 ) (2)
kk
kk
f f A
f f B B
⊙ Eduardo E. Cabezas, Diego J. Celentano, 2004, Experimental and numerical analysis of
the tensile test using sheet specimens, SAE 1045 steel.
Cylindrical specimen Sheet specimen
New approach to material identification by tensile test
Elongation [mm]
Te
nsile
loa
d[k
N]
0 2 4 60
2
4
6
8
10
12
14
Measured
Prediction
Necking
point
Fracture
point
7.94
0x
0xy
0y
0yx
1/ 60mm/sy
0yx
( ) 0n
xt( ) 0n
yt
x
y
Gage
mark
Gage
mark
MS Joun et al., 2008, Mechanics of Material
-Material: SWCH10A
-Cylindrical specimen
-Iterative approach
-Rigid-plastic FEM
-Strength coefficient = function of strain
-Strain-hardening exponent
= true strain at the necking point
1.608E+0
1.407E+0
1.206E+0
1.005E+0
8.042E-1
6.032E-1
4.021E-1
2.011E-1
1.673E-7
Damage just before fracture
DCr=1.68
Elongation (mm)
Te
nsile
loa
d(N
)
0 2 4 6 8 100
5000
10000
15000
20000
25000
30000
35000
SCM435
ESW95
ESW105
⊙ Tensile load-elongation curves ⊙ True stress-strain curves
True strain (mm/mm)
Tru
estr
ess
(MP
a)
0 0.4 0.8 1.2 1.60
200
400
600
800
1000
1200
SCM435
ESW95
ESW105
Applications of the new approach to material ID
Engineering strain (mm/mm)
En
gin
ee
rin
gstr
ess
(MP
a)
0 0.1 0.2 0.3 0.40
200
400
600
800
1000
1200
Experiment (SCM435)
Analysis (SCM435)
Experiment (ESW95)
Analysis (ESW95)
Experiment (ESW105)
Analysis (ESW105)
Applications of the new approach to material ID
Verification of predictions
PredictionExperiment
SCM435 ESW105
Non-contacted Contacted Non-contacted Contacted
By AFDEX
A general-purpose metal forming simulator based on rigid or elasto-thermoviscoplastic FEM
Research objective
○ Suggestion of an improved approach to finite element prediction
of central bursting defects.
-Rigid-plastic FEM
-Improved node separation scheme
-Damaged element removal scheme
○ Parametric studies for revealing the effects of process design
parameters on the chevron defects.
-Effect of reduction of area
-Effect of die conical angle
-Effect of friction
-Effect of strain-hardening exponent
An improved element split scheme
Step 1. Set i=0
Step 2. Select the most damaged element ⓘ
Step 3. Find the most damaged edge ⓘ on the boundary of the element ⓘ
Step 4. Set i=i+1 and go to Step 2
I
J K
Komori first applied the element split scheme
Element elimination or degredation schemes
②
① ②
③
① ②
③
①
③ ④
④
Komori Present
Before After
Damaged element cleaning scheme
Damage model used
1
0
f
D d
0
f
D d
McClintock damage model
Special case of McClintock damage model, employed in this study
1.0, / 2n
2.13E-001
1.46E-001
7.96E-002
1.30E-002
C L
1.52E+000
1.23E+000
7.84E-001
4.89E-001
3.42E-001
1.23E-002
Metal flow Distorted mesh Damage Effective strain
Example
1 3 1 32
sinh[ 3(1 ) ]3(1 )
nn
Cases of extrusion process designs, simulated
Finite element model Punch
Die
● Workpiece size: Φ14.0 mm × h 28.7 mm ● Strain hardening exponent: 0.14 ● Critical damage: 0.20 ● Initial mesh size: 0.2 × 0.2mm ● Number of quadrilateral elements: 4862
Workpiece
Angle, α [ º] Reduction of area, R.A. [%] Coefficient of
Coulomb friction, μ
Case 1 30 18 0.03
Case 2 60 18 0.03
Case 3 30 30 0.03
Case 4 30 18 0.05
2
Angle, α [ º] Reduction of area, R.A. [%]
Coefficient of Coulomb friction,
μ R.A 60 18 - 39 0.05
Conical angle 30 - 100 25 0.03
Friction 60 30 0.01 - 0.1
General cases
Parametric studies
General cases
(a) Case 1 (b) Case 2 (c) Case 3 (d) Case 4
30, 18,
0.03
60, 18,
0.03
30, 30,
0.03
30, 18,
0.05 αº, R.A.%,
μ
82r 89r 68r 87r
82meanr
Effect of reduction of area (α=60º, μ=0.05)
R.A.=18.0 R.A.=25.0 R.A.=30.0 R.A.=39.0
87r 86r 77r 55r
Experimental results of Zimerman et al. [22].
When R.A. is greater than a certain value, the smaller R.A., the more dangerous
Effect of die angle (R.A.=18%, μ=0.03)
α= 30º α= 60º α= 80º α= 100º
82r 89r 87r 82r
Similar numerical results for die conical angles of less than 60°
by Saanouni et al. [4]
The same as experimental research works of Zimerman et al. [22]
and numerical study of Aravas [23].
Effect of friction (α= 60º, R.A.=18%)
010.μ 050.μ 100.μ . 0 15μ
92r 87r 86r 0r
Similar numerical studies by Saanouni et al. [4] and Soyarslan et al. [5]
Conclusions
⊙ A new scheme of predicting crack propagation was presented. -An improved element split -A critical case of Mcklintock’s damage model
-Rigid-plastic FEM -Damaged element cleaning scheme ⊙ Central bursting defect was successfully simulated by the new scheme. -The normalized crack radius, ratio of chevron defect’s radius to extrusion
radius is large compared with other researches -Defect shape is also different from others ⊙ Effects of Coulomb friction, die angle and reduction of area were investigated. -Nearly the same as the previous stuides, but they are so complicatedly coupled that additional studies should be accomplished.
○ Material: SWCH10A
○ DCr=1.68
A
C B
12.5slope
0.002
12.5slope
0.002
Recent work on fracture prediction in tensile test
O
Elongation [mm]
Te
nsi
lelo
ad
[kN
]
0 1 2 3 4 5 6 7 8 90
2
4
6
8
10
12
ExperimentPrediction
A
C
B
O
B
C
O A B
Damage model used
1
0
f
D d
0
f
D d
McClintock damage model
Special case of McClintock damage model, employed in this study
1.0, / 2n
2.13E-001
1.46E-001
7.96E-002
1.30E-002
C L
1.52E+000
1.23E+000
7.84E-001
4.89E-001
3.42E-001
1.23E-002
Metal flow Distorted mesh Damage Effective strain
Example
1 3 1 32
sinh[ 3(1 ) ]3(1 )
nn
Effect of die conical angle on damage
Half die conical angle (degree)
Ma
xim
um
cu
mu
lative
da
ma
ge
0 10 20 30 40 500
0.1
0.2
0.3
0.4
0.5
0.6n=0.001
n=0.05
n=0.10
n=0.15
n=0.20
n=0.25
30%R.A. =
30
Reduction of area (%)
Ma
xim
um
cu
mu
lative
da
ma
ge
0 10 20 30 40 500
0.1
0.2
0.3
0.4
0.5
0.6n=0.001
n=0.05
n=0.10
n=0.15
n=0.20
n=0.25
Effect of reduction of area on damage
Half conical angle =
Effect of friction on damage
Friction coefficient
Ma
xim
um
cu
mu
lative
da
ma
ge
0 0.05 0.1 0.15 0.20
0.2
0.4
0.6
n=0.001
n=0.05
n=0.10
n=0.15
n=0.20
Coefficient of Coulomb friction
30%R.A. = 30Half conical angle =