Modeling Loss-of-Flow Accidents and Their Impact on Radiation Heat Transfer

Table 8

Sample tuned parameters.

Component	Mass flow rate (kg/s); (designed value)	Temperature (K); (designed value)	Pressure (MPa); (designed value)
Reflector exit	13.65 (13.65)	126.27 (125.00)	5.58 (5.71)
Core inlet	14.06 (14.06)	118.50 (127.78)	5.44 (5.56)
Core exit (including ICC, HCC, PCC, M1, slat, annulus, and tie rod)	18.60 (18.59)	1767.08 (1755.23)	4.19 (4.28)
Fuel element exit (including ICC, HCC, and PCC)	11.86 (12.13)	2619.53 (2555.56)	4.19 (4.28)

The second entry in parenthesis is the design value for each case.