Cast Stainless Steel
Modelling of Ultrasonic Propagation in Cast Stainless Steels with Coarse Grained Structures F. Jenson, L. Ganjehi and C. Poidevin, CEA, LIST, France
G. Cattiaux and T. Sollier, Institut de Radioprotection et de Sûreté Nucléaire, France
ASBSTRACT
Cast stainless steel (CSS) material has been used extensively in the primary loop of French pressurized
water reactors (PWR). Due to their particular metallurgical structure, the ultrasonic inspection of CSS
components is very challenging. As it propagates thru the structure, the transmitted field is strongly
affected by the anisotropic behaviour of the macrograins constituting the metallurgical structure. This
can lead to beam distortions and disruptions, and consequently to severe limitations of inspection
performances. In this study, an approach is proposed in order to compute wave propagation in
heterogeneous materials such as CSS. In a first step, the geometrical properties of the large scale
structure are mimicked using Voronoi diagrams. Secondly, the elastic properties of the macrograins
are estimated using a Voigt homogenization procedure applied to the colonies. Finally, the wave is
propagated thru the structure using the pencil method. For validation purpose, measurements were
performed on a pipe segment that is believed to be representative of centrifugally cast stainless steel
materials used in PWR. The back wall and corner-trap echoes were measured by scanning the probe
over large areas. It is shown that important experimental phenomena such as amplitude and time of
flight fluctuations can be reproduced thanks to the approach proposed in this paper.
CONTEXT
CSS components are made of a complex metallurgical structure. This structure exhibits very large
equiaxed or columnar grains (the so-called macrostructure). Due to their anisotropic elastic properties,
the beam transmitted thru the macrograins undergoes amplitude distortions and phase aberration. The
disruption of the transmitted field coherence properties will lead to weak inspection performances. For
instance, large notches (larger than the unperturbed beam size) will be missed in some sections of the
inspected component. The heterogeneous properties of the material will also lead to scattering of a
fraction of the incident energy in every direction of space. When measured by the receiver, the
scattered field is the source of a strong background noise also called structural noise (the modeling of
grain noise will not be addressed in this paper). Thus, the presence of a macrostructure is a limiting
factor of ultrasonic inspection capabilities and it must be accounted for when designing new NDE
methods. To assess the impact of large grain structures on ultrasonic beam propagation, CSS material
that represents those installed in primary piping circuits of French nuclear power plants was ordered.
An unflawed pipe section was available for the study. The geometrical properties of the specimen are
given in Figure 1.
40
0 m
m
937 mm
40
0 m
m
937 mm
40
0 m
m
937 mm
40
0 m
m
937 mm
75 mm
Figure 1 - CSS tube section used in the study.
Columnar
grains
Fine
equiaxed grains
Stratified
region
Mixed banded structure
Columnar
grains
Fine
equiaxed grains
Stratified
region
Mixed banded structure
Figure 2 - Macrographic pictures taken on various parts of the CSS tube section.
Areas in the circumferential-radial plane at one end of the piping segment were polished and
chemically etched to obtain photographs of the material structure. Figure 2 shows pictures resulting
from this process. The specimen contains a wide range of grain sizes and shapes. Overall, the structure
shows significant layering. This type of metallurgical configuration is a very challenging
macrostructure for ultrasonic examination because of the variability, size and layering of grains.
MODELS
Description of the macrostructure using Voronoi diagrams
As stated previously, the macrostructure is responsible of the beam distortions that are observed in
CSS materials. Since one of the objectives of this work is to model such structure induced
perturbations, the first step consists of describing the morphological properties of the various
macrostructures encountered in cast stainless steels. One simple way to achieve this is to use a
mathematical tool called Voronoi diagrams. Voronoi diagrams are decompositions of space in convex
cells. They give good qualitative representations of polycrystalline structures.
Figure 3 - Illustrations of Voronoi decompositions obtained using the Voronoi decomposition
algorithm proposed in the CIVA software
This approach has been conjointly proposed by EDF (Electricité de France) and CEA (the French
Atomic Energy Commission) in a previous paper [1] in order to model ultrasonic propagation in
coarse grained structures such has those found in cast stainless steels. The Voronoi decomposition
algorithm used in this study allows one to perform a 3D tessellation of cylindrical and planar shaped
specimens. The synthetic structure can be either constituted of equiaxed or columnar shaped grains. It
is also possible to define mixed-banded structures such as those shown in figure 2. Such structures are
very common in stainless steel components which are centrifugally cast. Illustrations of Voronoi
decompositions are shown in figure 3.
Description of the elastic properties of a macrograin
As stated previously, the anisotropic elastic properties of the macrograins disrupt the ultrasonic
propagation. Thus, it is important to accurately estimate the material properties of a single macrograin
constituting the macrostructure. Macrograins are made of an aggregate of bicrystals (colonies). These
colonies are, in turn, formed of an interconnected network of austenite and ferrite (see Figure 4). This
complex substructure appears during the cooling process by solid-phase transformation from the
ferritic to the austenitic phase. The colonies correspond to areas of about 1 mm where the austenitic
phase keeps the same crystallographic orientation. The crystallographic orientations of both phases are
related by the Kurdjumov-Sachs relationships. This gives 24 possible “variants” for each austenitic
grain orientation [2]. Starting from the elastic stiffness constants matrices of austenite and ferrite, it is
possible to express the elastic properties of the 24 variants in the lab coordinates. Then, assuming
equal probability for each variant within a macrograin, one can compute the ensemble average of the
elastic properties. This ensemble average simply consists of a Voigt average of the 24 elastic stiffness
matrices [3]. The results of this homogenization approach are given in Table 1.
Ferrite
Austenite
Ferrite
Austenite Figure 4 - Micrographic picture showing the interconnected laths of austenite and ferrite
122125198CγCristallite d’austénite
(cubique)
116134231CδCristallite de ferrite
(cubique)
441211Composante
122125198CγCristallite d’austénite
(cubique)
116134231CδCristallite de ferrite
(cubique)
441211Composante
96102254CM
Macrograin moyen
(cubique)96102254C
M
Macrograin moyen
(cubique)
Component
Ferrite (cubic)
Austenite (cubic)
Macrograin
(cubic)
122125198CγCristallite d’austénite
(cubique)
116134231CδCristallite de ferrite
(cubique)
441211Composante
122125198CγCristallite d’austénite
(cubique)
116134231CδCristallite de ferrite
(cubique)
441211Composante
96102254CM
Macrograin moyen
(cubique)96102254C
M
Macrograin moyen
(cubique)
Component
Ferrite (cubic)
Austenite (cubic)
Macrograin
(cubic)
Table 1 - Elastic stiffness matrices of the austenite, ferrite and homogenized macrograin
The corresponding anisotropic constants, defined as A=2C44/(C11-C12), are Aaustenite=3.34, Aferrite=2.39
and Amacrograin=1.26. Thus, anisotropy is much weaker in the macrograin due to the averaging process
than in the individual crystallites. Yet, fluctuations of quasi-longitudinal velocity must be taken into
account in our approach. This is done by randomly generating longitudinal wave velocities from a
uniform statistical distribution. The parameters of the distribution are the average L-wave velocity VL,
and the distribution width ∆VL. ∆VL controls the fluctuations of velocities from one macrograin to the
other. The larger the distribution width is, the larger the dispersion of velocity will be. The distribution
width can be estimated from the elastic properties of the homogenized macrograin. This is done by
solving the Christoffel equation for random orientations of the macrograin. This leads to a histogram
of possible qL-wave velocities from which the width of the uniform distribution is estimated.
Following this method, a value of ∆VL=2 % of the average velocity was obtained.
Computation of the transmitted beam using a pencil method
The next step was to simulate the ultrasonic field propagation in the Vornoi polycrystal. First, the field
radiated in the coupling medium by an arbitrary transducer is computed using the Rayleigh integral
model. The beam transmitted at any position in the macrostructure is then computed using the pencil
method [4] which is an extension of a ray theory [5]. Here, the macrostructure is modeled as an
aggregation of homogeneous volumes.
VL,i-1
VL,i
VL,i+1
Ti-1→i
Ti→i+1
Transmission
coefficients
Refraction + divergence
VL,i-1
VL,i
VL,i+1
Ti-1→i
Ti→i+1
Transmission
coefficients
Refraction + divergence
Figure 5 - Computation of the transmitted beam using the pencil method.
Therefore, the propagation from the transducer to a specific position in the specimen involves
transmission and reflection at several interfaces (see Figure 5). The propagation of the central ray of a
pencil is governed by the geometrical optics laws. As the pencil is propagated through a succession of
interfaces, the wavefront deformation is also taken into account. Thus, this method can be computed
using an iterative algorithm and is well adapted to model wave propagation in heterogeneous media.
EXPERIMENTAL STUDIES
Experimental setup for the measurement of the back wall and of the end-of-block corner echoes
Two large aperture 1 MHz focused probes were used during the acquisition process. The first one was
dedicated to the back wall echo measurements and the second one to corner echo measurements. The
probes were positioned from the outside-diameter surface, such as to produce 0° and 45° refracted
beams focused near the inner surface of the specimen. The objective was to target the back wall and
the inside-diameter corner at the end of the segment. The transmitted beams for both cases were
simulated in a homogeneous stainless steel specimen. Results are shown in Figure 6 along with
illustrations of the experimental setups. The simulation ensures that the probes are capable of
producing a correct insonification in the areas of interest, thus at a depth of about 75 mm and with a
45° refracted angle for corner echo measurements. A 2D scan was acquired over a 60 mm long axial
displacement and a 320° circumferential rotation around the end-of-block corner. The back wall echo
was acquired over a 330 mm long axial displacement and a 355° circumferential rotation.
33
0 m
m
Z
θ: 0°→ 355°
75 m
m
60 mm
Rotation
Displacement
320°
Figure 6 - Experimental setup for the back wall echo (upper figure) and for the end-of-block corner
echo (lower figure) measurements
Estimation of quantitative parameters
Several quantitative parameters were defined and estimated from the experimental results. These
parameters are useful to perform quantitative comparisons between experimental and simulation
results. The first of these parameters consists of the averaged amplitude of the back wall response
determined with several probe positions. This amplitude is then compared to that of an echo measured
on a standard reflector located in a reference specimen (here, a side drilled hole positioned at a depth
of 75 mm in a homogeneous and non-attenuating specimen). Another parameter was defined and used
to characterize the back wall signal fluctuations. It is computed from the standard deviation of the set
of values that is formed from the measurement of the back wall signal amplitude for each probe
position. This value is then compared to the mean amplitude value that was previously defined and
computed. Table 2 shows results for the two parameters estimated on three distinct angular sections of
the experimental C-scan. These results show strong variations from one region to the other.
-8,2
22
-8,0
31
[40 80]
-4,8
13
Average amplitude [dB]
Amplitude fluctuations [%]
Angular section [100 135] [165 220]
Table 2 - Experimental values of the quantitative parameters characterizing the back wall response
C-scanEcho-dynamic
Blow-up
C-scanEcho-dynamic
Figure 7 - Left figures: Assessment of the baseline ultrasonic noise level. The corner response from
the pipe segment is shown on the left; grain noise with no geometrical reflectors is shown in the
middle; echo-dynamic showing the maximum amplitude of the noise for each incremental position is
shown on the right. Right figures: Determination of the detection percentage calculated from the total
specimen length scanned. The detection threshold corresponds to maximum amplitude of the grain
noise (blue line)
Quantitative parameters characterizing the corner echo signal and the inherent structural noise were
also assessed. The C-scan data was evaluated for signal and noise information as well as the presence
or absence of the corner-reflected signal. First, an assessment of the baseline ultrasonic noise level in
the specimen was made by processing the signal acquired for probe positions far enough from the end
of block so that no corner-trap response could contribute. This step is illustrated in Figure 7. The
corner-trap is detected with a maximum signal-to-noise ration of 5 dB. Yet, a loss of the corner-trap
response is observable for several angular positions of the probe. An analysis of the C-scan data was
conducted to quantify the detection percentage of the total specimen length scanned. The noise level
previously assessed was used to fix a detection threshold. The analysis performed on the results in
Figure 7 gave a detection percentage of 64 %. This result illustrates the strong impact of the
metallurgical structure on the detection performances. Note that the corner-trap represents a 100 %
through-wall flaw. Thus, it can be seen as a perfect ultrasonic inspection reflector.
COMPARISONS WITH SIMULATION RESULTS
Simulation of the transmitted beam
The radiated beam was computed for both L0 and L45 configurations. The input parameters of the
simulation were ∆VL=2 % and a mean grain size of 14 mm. The radiated beam was also computed for
a homogeneous and non attenuating specimen. As it is shown in Figure 8, the presence of a Voronoi
diagram strongly disrupts the transmitted beam.
L0
Homogeneous
Voronoi
Mean grain diameter:
14 mm
L45
Figure 8 - Simulation of a beam radiated thru a homogeneous (left) and a coarse grained (right)
specimen.
Simulation of the back wall response
The back wall echo was computed for several probe positions allowing to display B-scans in a similar
way to those measured experimentally. The results are shown in Figure 9. The input parameters of the
simulation were ∆VL=2 % and a mean grain size of 12 mm. Both the amplitude and time-of-flight
fluctuations are well reproduced. The morphological properties of the macrostructure were unknown
when the study was performed. Thus, a sensitivity study on the mean cell size of the Voronoi diagram
was performed. For each input value, the simulation was carried out and the quantitative parameters
were estimated. The results of the study are plotted in Figure 10.
Displacement
Tim
e
Displacement
Tim
e
Displacement
Displacement
Am
pli
tud
eA
mp
litu
de
Displacement
Tim
e
Displacement
Tim
e
Displacement
Displacement
Am
pli
tud
eA
mp
litu
de
Sim
ula
tio
nE
xp
eri
men
tal
Figure 9 - Simulation and experimental results of the back wall response.
-10
-5
0
5
10
15
20
0,0 1,0 2,0 3,0 4,0 5,0
Mean grain size [cm]
Me
an
am
pli
tud
e [
dB
]
Mean amplitude Amplitude fluctuations
0
5
10
15
20
25
30
35
0,0 1,0 2,0 3,0 4,0 5,0
Mean grain size [cm]
Am
plitu
de f
luctu
ati
on
[%
]
Experimental results
Experimental results
Simulation results
Simulation results
Figure 10 - Mean echo amplitude and amplitude fluctuations as a function of the mean grain size:
Simulation (▲marks) and experimental (lined band) results
The results show that the mean amplitude tends to increase with the grain size. As described in a
previous paper [1], this relationship can be predicted by theoretical models for frequencies
corresponding to the geometrical domain, i.e. when the wavelength is larger than the typical grain size
of the metallurgical structure [6,7]. Yet, simulation seems to overestimate the mean amplitude since
the experimental values are lower then the simulation even for a mean grain diameter of 0.5 cm. This
result shows that additional sources of attenuation may be needed to complement the approach. For
instance, the losses due to the interaction of the beam with the substructure could be evaluated by
computing the attenuation coefficient due to the substructure only. Another interesting result concerns
the particular bell shape of the relationship between the back wall signal fluctuations and the mean
grain size. The fluctuations are weak for either small or large grains, going thru a maximum value
obtained for a particular grain size. This result is quite intuitive since the structure can be considered to
be homogeneous for the wave propagation when the grains are either very small or very large when
compared to the wavelength. The results also show that experimental values of the amplitude
fluctuations can be reproduced for particular values of the input parameter.
Simulation of the corner-trap response
The corner echo was also computed for several probe positions. Here, the displacement was made in
the rotational direction. The results are shown in Figure 11. The input parameters of the simulation
were ∆VL=2 % and a mean grain size of 12 mm.
rotation (°)
time (µs)
180 185 190 195 200 205 210
88
88.5
89
89.5
90
90.5
91
91.5
92
180 185 190 195 200 205 210-10
-9
-8
-7
-6
-5
-4
-3
-2
-1
0
rotation (°)
Amplitude (dB)
rotation
Tim
eA
mp
litu
de
Tim
eA
mp
litu
de
rotation
Figure 11 - Experimental (left) and simulation (right) results of the corner response.
The strong amplitude and time-of-flight fluctuations are predicted by the model. Yet, quantitative
comparisons such as those performed on the back wall echo must be realized to complement the
validation work. For instance, C-scans such as those shown in the Figure 7 must be computed in order
to obtain an accurate estimation of the detection percentage. Since structural noise is not modeled in
this approach, the detection threshold must be fixed from the experimental noise level. These studies
are currently under way.
CONCLUSIONS
A method was proposed in this paper in order to model fluctuations of the transmitted beam induced
by the metallurgical structure of cast stainless steel. This method is based on a description of the
morphological properties of the macrostructure using Voronoi diagrams. The elastic properties of the
macrograin are obtained from a homogenisation of the substructure which is made of colonies of
austenite. An isotropic assumption is made for computational efficiency purpose and the transmitted
beam is obtained using a pencil model. This algorithm allowed us to reproduce the fluctuations in
amplitude and time of flight of the back wall and end-of-block corner-trap responses. Additional
sources of attenuation are required to accurately predict the losses incurred by the propagating field.
ACKNOWLEDGMENTS
This work has been funded as part of a collaborative project between the US NRC and the IRSN. The
objectives of this project are:
• To improve and/or develop and validate simulation to get a better understanding of the effect
of grain structures on ultrasonic propagation.
• To assess a large number of CSS materials, maximising de variability of macrostructures.
• To develop new efficient phased array techniques for application on CSS, taking into account
the simulation studies.
REFERENCES
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effect in ductile fracture: application to thermal embrittlement of duplex stainless steels”,
Engineering Fracture Mechanics, 67, pp. 169-190.
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microstructures: theory and application to titanium alloys”, Metallurgical and Material
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