CFD Applications to Pressurized Thermal Shock-Related Phenomena

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijer/volume-2024/5114542/figures/5114542.fig.006a.svgz" name="5114542.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Thermocouple lance locations in the CL (left) and the DC (right) [<a href="/journals/ijer/2024/5114542/#B15">15</a>]</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijer/volume-2024/5114542/figures/5114542.fig.006b.svgz" name="5114542.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Normalized temperature distribution in the CL (upper) and the DC (lower) [<a href="/journals/ijer/2024/5114542/#B17">17</a>]</td></tr></table>

<div>Comparison with the experimental result on the SSSW 3-17 case in TOPFLOW-PTS conducted in the NURESAFE project.</div>

International Journal of Energy Research

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Figure 6

Figure 6: CFD Applications to Pressurized Thermal Shock-Related Phenomena 