Table 6 Critical values for post-hoc tests after the Friedman test.

From: Enhancing grasshopper optimization algorithm (GOA) with levy flight for engineering applications

#classifiers

2

3

4

5

6

7

8

9

10

q0.05

1.96

2.343

2.569

2.728

2.85

2.949

3.031

3.102

3.164

q0.10

1.645

2.052

2.291

2.459

2.589

2.693

2.78

2.855

2.92

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