Boundary conditions for the numerical study.
|Pressure outlet po (MPa)||0.1, 0.5, 1.5, 2.0, 2.5, 3.5, 4.5|
|Mass flow rate inlet q (kg/s)||0.051, 0.06, 0.19,|
|Heat source Ts (K)||900, 1073, 1100|
|Rotor speed n (rpm)||50000|
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