Advances in Aerodynamics

Table 2 The original 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
No	x/c = -0.5	-0.4375	-0.375	……	0.375	0.4375	0.5	C_Lmax	Stall α
1	0	0	0	……	0	0	0	1.221	22
2	0.0225	0.0225	0.0225	……	0.0225	0.0225	0.0225	1.178	24
3	0.0275	0.0225	0.0125	……	0.0125	0.0225	0.0275	1.170	24
4	0.0275	0.0225	0.0075	……	0.0225	0.0225	0.0225	1.178	24
5	0.0325	0.0225	0.0075	……	0.0075	0.0225	0.0325	1.133	24
6	0.0225	0.0275	0.0225	……	0.0225	0.0125	0.0225	1.195	22
7	0.0125	0.0225	0.0275	……	0.0275	0.0225	0.0125	1.221	24
8	0.0225	0.0125	0.0225	……	0.0225	0.0275	0.0225	1.251	24
9	0.0275	0.0125	0.0125	……	0.0125	0.0125	0.0275	1.176	23
10	0.0325	0.0125	0.0125	……	0.0125	0.0125	0.0325	1.173	23
11	0.0125	0.0275	0.0125	……	0.0125	0.0125	0.0125	1.205	23
12	0.0125	0.0125	0.0275	……	0.0275	0.0125	0.0125	1.242	24
13	0.0125	0.0125	0.0125	……	0.0125	0.0275	0.0125	1.207	23

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