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ENSI Erfahrungs- und Forschungsbericht 2011
netics is strongly dependant, especially at high
temperature, upon the initial oxide layer thickness
and therefore, uncertainties in measured data
(with regards to the pre-oxide layer thickness in
both axial and azimuthal directions) makes it diffi-
cult to fully assess the obtained code results. Fur-
thermore, some cracks were found in the oxide
layer, something that was so far not considered
in the FALCON analyses. These studies are there-
fore planned to be continued in the perspective
of further enhancing the FALCON code predictive
capabilities related to both oxidation kinetics as
well as hydrogen pickup during accidents in gen-
eral and LOCAs in particular.
Fuel behaviour during reactivity-initiated-
accidents
Related to fuel safety criteria for reactivity-ini-
tiated-accidents (RIAs), an OECD/CSNI RIA code
benchmark was initiated during 2011 with the
objective to assess the reliability of fuel behav-
iour codes to reproduce the results of RIA tests
conducted at the IRSN CABRI and JAEA NSRR test
reactors. Within STARS, the objective is to partici-
pate to this benchmark with FALCON coupled to
GRSW-A in order to further address and under-
stand the role of transient gaseous swelling under
RIA conditions. Consequently, a first series of se-
lected CABRI tests were modeled and the analysis
results were presented at a recent meeting of the
OECD-CSNI Work Group for Fuel Safety (WGFS).
In spite of a considerable scatter in the solutions
obtained by the different participants, the PSI re-
sults using FALCON with GRSW-A were found to
yield feasible estimations of FGR, fuel and cladding
temperatures, cladding failure and residual hoop
strain for the CABRI CIP01 case. Indeed, as shown
on the left-hand side of Fig. 10, the predicted axial
profile of the residual cladding hoop strain shows
a rather good agreement with the corresponding
measurement.
On the other hand, the PSI predictions stood apart
from other solutions with respect to the cladding
elongation that occurred during this test. The rea-
son for this was recently found to be an inadequate
restart option in the current FALCON scheme for
base irradiation including fuel refabrication. To
overcome this, an alternative scheme was applied,
resulting in a much better agreement with mea-
surements and showing at the same time, as illus-
trated on the right-hand side of Fig. 10, an impor-
tant impact from the predicted gaseous swelling for
a successful interpretation of the measured data.
Multi-physics and coupling methodologies
One central mission of STARS is to develop multi-
scale and multi-physics computational method-
ologies to improve the reliability of models and
simulations applied for transient/accident safety
evaluations. During 2011, emphasis was given
to multi-physics activities aimed at establishing
numerical coupling schemes between simulation
codes handling different physical domains (e.g.
thermal-hydraulics, neutronics, thermo-mechan-
ics) in order to take into account the relevant
spatial/temporal feedback occurring between the
governing physical phenomena handled by each
stand-alone code.
Figure 10:
Modeling and Analysis
with FALCON coupled to
GRWS-A of CABRI CIP01
Test.
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