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Advances in Aerodynamics

Table 3 The discrete decision information table

From: Effect of vortex generator spanwise height distribution pattern on aerodynamic characteristics of a straight wing

No

C1

C2

C3

……

C15

C16

C17

D1

D2

x/c = -0.5

-0.4375

-0.375

……

0.375

0.4375

0.5

CLmax

Stall α

1

1

1

1

……

1

1

1

2

0

2

3

3

3

……

3

3

3

1

2

3

3

3

2

……

2

3

3

1

2

4

3

3

2

……

2

3

3

1

1

5

3

3

2

……

2

3

3

1

2

6

3

3

3

……

3

2

3

1

0

7

2

3

3

……

3

3

2

2

2

8

3

2

3

……

3

3

3

3

2

9

3

2

2

……

2

2

3

1

1

10

3

2

2

……

2

2

3

1

1

11

2

3

2

……

2

2

2

2

1

12

2

2

3

……

3

2

2

3

2

13

2

2

2

……

2

3

2

2

2

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