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 parameters | Value |
| 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 |
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