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Table 1 Experimental state

From: Experimental study on transition of dynamic airfoil in pitching oscillation

Case

c/mm

Re/106

k

α0

A

1

700

1.5

0.069

5

15

2

700

1.5

0.035

15

10

3

700

1.5

0.050

15

10

4

700

1.5

0.069

15

10

5

700

1.5

0.100

15

10

6

700

1.5

0.139

15

10