Research Article

Investigation of Rotating Stall Phenomenon and Optimization in Mixed-Flow Waterjet Propulsion Device

Table 5

Total pressure coefficient on each section.

Original schemeSelected scheme
0.5 Q′0.67 Q′Q′0.5 Q′0.67 Q′Q′

Total pressure coefficientSection 5-50.29700.29560.29500.29790.29770.2966
Section 4-40.28840.28940.29080.28390.28820.2908
Section 3-30.28550.28760.29030.28060.28570.2876
Section 2-20.36650.37120.35150.36520.36650.3515
Section 1-10.35800.36300.34530.35620.35820.3446