CFD Applications to Pressurized Thermal Shock-Related Phenomena

Figure 5

Comparison with the experimental result on d10m10 in ROCOM conducted in the IAEA CRP.

(a) Upper downcomer sensor locations [81]

(b) Local MS at the position of the center of the CL (circumferential angles of 22.5°) in the upper DC sensor [30, 32, 80, 81]