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8/12/2019 A New Yield Function for Porous Materials
1/8
Journal of Materials Processing Technology 179 (2006) 3643
A new yield function for porous materials
Lus M.M. Alves, Paulo A.F. Martins, Jorge M.C. Rodrigues
Institute Superior Tecnico, Departamento de Engenharia Mecanica, Av. Rovisco Pais, 1049-001 Lisboa, Portugal
Abstract
Densification of sintered copper under uniaxial compression is analyzed by means of three different plasticity criteriaShima and Oyane [S.
Shima, M. Oyane, Plasticity theory for porous metals, Int. J. Mech. Sci. 18 (1976) 285291], Doraivelu et al. [S.M. Doraivelu, H.L. Gegel, J.S.
Gunasekera, J.C. Malas, J.T. Morgan, J.F. Thomas, A new yield function for compressible P/M materials, Int. J. Mech. Sci. 26 (9/10) (1984)
527535] and Lee and Kim [D.N. Lee, H.S. Kim, Plasticity yield behaviour of porous metals, Powder Metall. 35 (1992) 275279]. Theoretical
predictions are compared with experimental data and served as a basis for developing a new yield function for compressible P/M materials. The
proposed yield function is not only capable of providing a better agreement with the experiments as its implementation into an existing finiteelement computer program proves to be successful for the numerical modelling of a powder forged component.
2006 Elsevier B.V. All rights reserved.
Keywords: Powder forging; Finite element method (FEM); Experimentation
1. Introduction
Recent advances in computing technology and reduction in
the associated costs are presently extending the availability of
computer programs to simulate complex P/M forming processes.
At present time computer programs have the potential to accu-rately model complex three dimensional P/M processes without
the need to take advantage of possible geometrical and material
flow simplifications.
Most of the scientific and numeric ingredients which are
necessary to develop and utilize these programs (discretization
procedures, solution techniques, contact algorithms and remesh-
ing schemes) are now nearly established but other important
ingredients, probably even more relevant than the former, to
the progress of numerical simulation, still deserve attention.
The yield function and its associated constitutive equations for
porous materials [1,2] is oneof these ingredients because it plays
a crucial role in the overall performance of the computer pro-
grams.
This paper is based on a comprehensive investigation of the
commonly used yield functions due to Shima and Oyane [3],
Doraivelu et al.[4]and Lee and Kim [5].The main objective
was to characterize and understand its limitations but also to
develop a new more accurate one if necessary.
Corresponding author. Fax: +351 21 841 90 58.E-mail address:[email protected](J.M.C. Rodrigues).
The most important drawback in the utilization of the above-
mentionedyieldfunctions is dueto thefact that theinitial relative
density does not explicitly influence the geometric hardening of
the base material and the plastic Poisson coefficient. Some of
the yield functions cannot even be used when the initial relative
density of the preforms is low.The paper deals with these problems and proposes a new
yield function for powder materials that takes into account the
initial relative density of thepreform. New testing procedures for
characterizing the mechanical behaviour of the base material are
also introduced in order to obtain a more accurate stressstrain
curve of the powder material.
The implementation of the new proposed yield function into
an existing finite element computer program is also briefly con-
sidered and assessment is provided by means a numerical and
experimental study of a powder forging process. To this end, a
laboratory controlled test comprising the forging of a sintered
copper perform was designed in such a way that material flow
behaviour, geometric profile, distribution of relative density and
forging load, could be reproduced and compared against numer-
ical estimates.
2. Theoretical background
The yield function for porous materials differs from the von
Mises function for dense materials due to the changes produced
in the volume of the porous bodies during plastic deformation.
In general, considering that the material is isotropic, and that the
0924-0136/$ see front matter 2006 Elsevier B.V. All rights reserved.
doi:10.1016/j.jmatprotec.2006.03.091
mailto:[email protected]://localhost/var/www/apps/conversion/tmp/scratch_4/dx.doi.org/10.1016/j.jmatprotec.2006.03.091http://localhost/var/www/apps/conversion/tmp/scratch_4/dx.doi.org/10.1016/j.jmatprotec.2006.03.091mailto:[email protected]8/12/2019 A New Yield Function for Porous Materials
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L.M.M. Alves et al. / Journal of Materials Processing Technology 179 (2006) 3 643 37
Table 1
The parametersA,B and for different porous yield functions
A B
Shima and Oyane[3] 31+(2.49/3)2(1R)1.028
(2.49/3)2 (1R)1.0281+(2.49/3)2 (1R)1.028
R5
1+(2.49/3)2 (1R)1.028
Doraivelu et al.[4] (2 +R2) (1R2 )
3 (2R2 1)
Lee and Kim[5] (2 +R2) (1R2 )
3
(RRc )2
(1Rc)2
deformation does not produce anisotropy, the yield function for
porous materials must include the first invariant I1of the stress
tensor and the second invariant of the deviatoric stress tensorJ2[1,2],
AJ2 + BI21= 20= 2R (1)The yield function for porous materials represents in the prin-
cipal stress space, the surface of an ellipsoid that is symmetrical
with respect to the three principal stress axes and has a major
axis that coincides with the mean stress axis. The parameters
A, B and are to be determined from experimental work andmust be expressed as functions of the relative density R (ratio
of the volume of the base material to the total volume of porous
material). The symbol R denotes the apparent yield stress of
the porous material which depends on the yield stress 0of the
base material and the relative density R.
Considering the porous material as a continuum medium,
the strain-rate components can be obtained from the associated
porous flow rule(1)as follows[7],
ij=R
R
A
2ij+ (3 A)mij
(2)
where m is the apparent mean stress and R is the apparenteffective strain rate of the porous material given by,
R=
2
Aij
2 + 13(3 A)
2v
1/2(3)
The symbol v= R/R refers to the volumetric strain-rate(ratio of the rate of variation of the relative density to the relative
density) and the apparent effective stress Ris determined by,
R=
(AJ2 + BI21 ) (4)The plastic deformation of a porous material includes two
different forms of hardening; (i) geometric hardening due to
material densification (parameter in Eq.(1))and (ii) materialhardening due to changes in the mechanical properties of the
base material (the yield stress 0 of the base material). The
relation between the apparent strain and strain-rate and those of
the base material can be obtained by combining the plastic work
rate,
w = R RVR= 0 0V0= 0 0RVR (5)with the geometric hardening parameter resulting from mate-
rial densification,
0
=
RR 0
= t
0
0dt
= t
0
R0dt (6)
Table 1summarizes the parameters A, B and of the yield
functionsthat were proposed by Shima andOyane[3], Doraivelu
et al.[4] and Lee and Kim[5].These functions are commonly
utilized in thenumerical simulation of porousmetal forming pro-
cesses and turn into the conventional von Mises yield function
for dense materials as the relative density R approaches unity.
In these limiting conditions ( = 1), the total apparent energy
of deformation becomes equal to the elastic energy of distortion
(becauseA =3andB = 0). Itis alsoimportantto notefromTable 1
that the yield function proposed by Doraivelu et al. cannot be
applied for values of the relative density Rc 1/2 = 0.71and that the yield function due to Lee and Kim makes use of
a critical relative density Rc that needs to be determined from
experiments.
The numerical simulation of P/M metal forming processes
starts from the following weak variational form expressed
entirely in terms of the arbitrary variation in the velocity u,
=
V
R RdV
S
FiuidS= 0 (7)
where V is the control volume of the porous body limited by
surfacesSu and SF, where velocity u i and traction Fi are pre-
scribed, respectively. The solution of Eq. (7) by thefiniteelementmethod requires subdivision of the control volume Vby means
ofMelements linked through Nnodal points. In each element
the velocity distribution can be represented in the vectorial form
as,
u = Nv (8)
whereN is the matrix containing the shape functions Ni of the
element and v is the nodal velocity vector. The strain rate vector
can be obtained from,
= Bv (9)whereB is the velocity strain rate matrix. Substituting Eqs.(8)
and(9)into Eq.(7)at the elemental level and assembling the
element equations with global constraints, it follows,
Mm
V(m)
RR
Kv dV
S(m)NF dS
= 0 (10)
whereK = BTDBandDis a matrix resulting from the inversion
of the porous constitutive Eq.(2).Further details on the imple-
mentation of the finite element method for P/M metal forming
processes can be found elsewhere[6,7].
8/12/2019 A New Yield Function for Porous Materials
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38 L.M.M. Alves et al. / Journal of Materials Processing Technology 179 (2006) 3643
Fig. 1. Scanning electron micrographs of the copper powder utilized in the experiments: (a) undeformed copper grains (magnification of 1000); (b) compacted andsintered copper grains (magnification of 4000).
3. Experimental work
3.1. Uniaxial compression test
Thematerialemployed in theexperimentswas a purecopperpowder(99.5%)
withan apparentdensityof 2.86g/cm3 andthe followingdistributionof grainsize
(obtained by means of sieve analysis): 94.92% 45m, 5.08% 45m and0% 75m.Fig. 1presents two photomicrographys of the material showingthe original (Fig. 1(a)) and the deformed powder grains (Fig. 1(b)) after being
compacted and sintered at 825 C, during 30 min in a vacuum atmosphere of0.55 mbar.
The experimental work was performed in a 500kN computer-controlled
hydraulicpress under a veryslow speed. The cylindrical compactedand sintered
specimens utilized in the uniaxial compression tests were produced in a double
effect tool, lubricated with zinc stearate, under different applied pressures in
order to ensure a good homogeneity and to obtain test specimens with different
values of the initial relative densityR0.Fig. 2presents some of these specimens
before and after being deformed.
In order to allow load recording during the test, force was applied to the
upper compression plate through one load cell based on traditional strain-gauge
technology in a full Wheatstone bridge. Displacements were measured using a
laser-based optical displacement transducer and a PC-baseddata logging systemwasused to recordand store loads anddisplacements. In addition to this, dimen-
sions and density of the compression test specimens were also measured at each
stepof deformation. Density wasmeasuredby means of a submersion technique,
using a precisionbalance with an accuracy of0.0001 g, andthe specimens hadto be previously waterproof sealed with a varnish of known density.
The compression tests were initially performed with the objective of inves-
tigating the consistency and accuracy of the aforementioned porous plasticity
criteria (Table 1)and of identifying a criterion to subsequent implementation
into an existing finite element computer program that is currently being devel-
oped within the research team. However, the study of the main features of these
criteria combined with some discrepancies that were found during its exper-
imental assessment stimulated the authors to develop a new porous plasticity
criterion. The criterion, entitled the initial density criterionIDC, considers,
Fig. 2. Compression test specimens made from compacted and sintered copper
powder before and after deformation. The labels 15 refer to specimens with
different values of the initial relative densityR0.
as the name indicates, the influence of initial relative densityR0 of the sintered
parts and will be presented in detail in the following sections.
3.2. Mechanical characterisation of the base material
The approach followed by the authors for the mechanical characteriza-
tion of the base material diverges from the commonly utilized methodology ofemploying a wrought material with identical chemical composition because the
metallurgical conditions play a crucial role in the overall mechanical response
of the materials. As shown inFig. 3the grain size of the wrought electrolytic
copper is much bigger than that of the compacted and sintered copper powder
with the same level of purity. Actually, this is one of the main advantages that
are usually attributed to the structural components produced by means of P/M
processes, because the reduced size of the powder grains is capable of ensuring
better mechanical properties whenever the overall level of porosity is reduced.
In order to overtake the inherent difficulties of obtaining the mechanical
characteristicsof thebasematerialby meansof directmethods, it wasdecidedto
develop a new indirect method based in compression tests, without friction, that
employscylindricalspecimens withdifferent valuesof theinitialrelative density.
Thecompression tests areperformed in such a waythateach incrementof stroke
Fig. 3. Micrographs showing the structure of: (a) a wrought electrolytic copper and (b) a sintered copper powder with equal purity. The magnification is equal to
400 in both cases.
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L.M.M. Alves et al. / Journal of Materials Processing Technology 179 (2006) 3 643 41
Fig.7. Powder forging of a copper flanged component. (ac)Initial, intermediate and finalgeometryof the flanged P/M component. (d) Correlation between measured
and computed geometrical profile of the cross section of the flange at three different stages of deformation.
all the porous plasticity criteria under investigation. The investigation made
use of test specimens with different initial densities and as it can be seen the
initial density criterion (IDC) is the only model that accurately reproduces the
mechanical behaviour of the sintered material for the test specimens with low
values of the initial relative densityR0 (Fig. 6(d)). In the case of the Doraivelu
et al. porous plasticity criterion it is not even possible to get an estimate for the
experimental test case performed with R0=0.686 because the critical relative
density of this criterion is higher Rc= 0.707> 0.686.
4. Powder forging of a flanged component
This section deals with the numerical modelling of the cold
powder forging of a copper flanged component and it was
included in the paper with the objective of validating the numer-
ical predictions provided by the finite element computer pro-
gram (modified in order to include the IDC porous criterion)
with the experimental measurements obtained from laboratory-
controlled conditions. Assessment is performed in terms of
material flow, geometrical profile, relative density and forging
load.
On account of rotational symmetry it was possible to carry
out the numerical simulation of the process under axisymmet-
rical modelling conditions. The initial cross section of the sin-tered preform (with an initial relative density R0= 0.79) was
discretized by means of a mesh consisting of 584 four-node
axisymmetric quadrilateral elements.Larger elements were used
to fill the body and the initial free regions of the preform whereas
the surfaces of interest (where contact is expected to occur) were
meshed with smaller elements in order to obtain more accurate
results on the filling behaviour. The contour of the dies were
approximated by means of contact-friction linear elements and
the friction factor was found to be equal to m = 0.2 in accordance
to a calibrationprocedurebased on the conventionalring-test [8].
Fig. 7 shows the geometry of the compacted and sintered pre-
forms that were used for producing the powder forged flanged
components together with deformed parts corresponding to the
intermediate and final stages of deformation. Geometry and rel-
ative density was also measured at these stages of deformation
and latter compared with the numerical estimates derived from
Fig.8. Powder forging of a copper flanged component. (a) Computedand exper-
imental evolution of the load vs. displacement; (b) computed and experimental
evolution of the average relative density vs. displacement.
8/12/2019 A New Yield Function for Porous Materials
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42 L.M.M. Alves et al. / Journal of Materials Processing Technology 179 (2006) 3643
finite elements. As seen fromFig. 7(d) the agreement between
the theoretical and experimental profiles is a very good.
Further assessment between computed and experimental
results can be found in Fig. 8, where the estimates of the
forging load and average relative density are plotted against
the correspondent experimental values. In case of the forging
load the agreement is excellent. Two different stages can be
identified; an initial stage where the evolution of the load is
Fig. 9. Computed and experimental distribution of the relative density. (ab) Computed distribution of the relative density at an intermediate stage of deformation
and at the final stage of deformation. (c) Micrographies showing the porosity in selected regions of the cross section of a component at the final stage of deformation.
Labels 115 refer to positions indicated in (b).
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L.M.M. Alves et al. / Journal of Materials Processing Technology 179 (2006) 3 643 43
smooth and similar to what is generally obtained for head-
ing operations with flat punches (although some radial flow
into the bottom of the preform begins at the early stages of
deformation), and a final stage where the forging load increases
sharply. The later starts when the die cavity commences to be
filled.
In what concerns the average relative density there is also
a good agreement between theory and experimentation but the
number of measurements and the average (integrator) charac-
teristics of the parameter are not adequate to conclude about the
overall quality of the finite element distribution of the relative
densityRinside the workpiece.
The above-mentioned limitations stimulated the authors to
perform a set of micrographies in selected regions of the cross-
section of the final flanged component and to compare theoreti-
calpredictionswith experimental observations. A closer analysis
ofFig. 9 enables to conclude that there is a good agreement
between the theoretical and experimental distribution of density
inside the workpiece and proves that the initial density criterion
IDC can be successfully applied in the numerical modelling ofP/M metal forming processes.
5. Conclusions
The porous plasticity criteria of Shima and Oyane, Doraivelu
et al. and Lee and Kim present difficulties in modelling the
mechanical behaviour of sintered parts with low values of the
initial relative density. This is due to the influence of the initial
relative density in the geometric hardening of the base material
and in the plastic Poisson coefficient.
The initial density criterion (IDC) that was proposed by
the authors takes this influence into account and proved tobe able to provide better estimates of the apparent field vari-
ables during the uniaxial compression of sintered copper powder
specimens.
A new indirect method for determining the stressstrain
behaviour of the base material was also proposed as an alter-
native to the commonly utilised approximate procedures based
on the utilization of wrought materials with similar chemical
compositions.
The implementation of the initial density criterion (IDC)
in a finite element computer program that is currently being
developed by the authors proved to be successful in the numer-
ical modelling of a powder forged component. Assessment is
provided by comparing finite element predictions of the mate-
rial flow, geometrical profile, relative density and forging load
against experimental measurements obtained from laboratory-
controlled conditions.
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