机翼攻角(˚)

升力系数(C_L)

阻力系数(C_D)

升阻比系数(C_L/C_D)

4.0

1.1050

0.0098

112.7551

4.5

1.1574

0.0101

114.5941

5.0

1.2092

0.0106

114.0755

5.5

1.2600

0.0110

114.5455

6.0

1.3059

0.0114

114.5526

6.5

1.3524

0.0119

113.6471

7.0

1.3985

0.0124

112.7823

7.5

1.4387

0.0132

108.9924

8.0

1.4565

0.0155

93.9677