Figures & data
Table 1. Primary geometric information of the centrifugal compressor.
Table 2. Domain grid node numbers.
Table 3. Relative errors of efficiency and head coefficient.
Note: A = the results without considering the mixing loss induced by the mixing plane method, meaning that the diffuser inlet parameters are taken from one plane after the interface between the impeller and the diffuser; B = the results considering the mixing loss caused by the mixing plane method, so the diffuser inlet parameters are taken from one plane before the impeller and diffuser interface; C = the time-averaged result of the unsteady calculations.