Table 3 Samples distribution based on DOE.
From: Influences of micro ramp vortex generators on the performance of flush waterjet propulsor
Case | Geometry | Performance | ||||||
|---|---|---|---|---|---|---|---|---|
H | A | L | S | \(\xi\) | \(\theta\) | DC60 | \(\eta\) | |
1 | 9.2 | 14.4 | 77.39 | 91.54 | 0.39 | 2.01 | 0.82 | 0.83 |
2 | 10.12 | 18 | 71.81 | 81.88 | 0.35 | 1.17 | 0.70 | 0.85 |
3 | 11.04 | 15.6 | 69.96 | 97.98 | 0.36 | 1.65 | 0.77 | 0.84 |
4 | 11.96 | 12 | 79.25 | 78.66 | 0.37 | 1.78 | 0.73 | 0.84 |
5 | 12.88 | 13.2 | 73.67 | 72.22 | 0.35 | 1.41 | 0.67 | 0.85 |
6 | 13.8 | 16.8 | 68.1 | 69 | 0.31 | 0.69 | 0.54 | 0.86 |
7 | 14.72 | 22.8 | 75.53 | 101.2 | 0.26 | 0.66 | 0.44 | 0.88 |
8 | 15.64 | 20.4 | 66.24 | 75.44 | 0.27 | 0.69 | 0.41 | 0.88 |
9 | 16.56 | 21.6 | 84.82 | 88.32 | 0.25 | 0.57 | 0.37 | 0.90 |
10 | 17.48 | 24 | 81.1 | 85.1 | 0.25 | 0.63 | 0.35 | 0.91 |
11 | 18.4 | 19.2 | 82.96 | 94.76 | 0.28 | 0.64 | 0.50 | 0.89 |
