Research Article

Experimental and Numerical Investigation of Temperature Distribution on Reactor Pressure Vessel Support under Operating Conditions

Table 1

The inlet cooling air parameters for an actual reactor support [22].

Inlet cooling air parametersValue

Heat loss(KW)40
Initial temperature(°C)27
Temperature rise causing by heat loss(°C)8.35
Final temperature(°C)35.35
Velocity (m/s)6.25