Appendix 1: Aerodynamic Drag Sample file.

0,0.091

0.2,0.091

0.5,0.091

0.7,0.091

0.8,0.092

0.85,0.10

0.9,0.122

0.92,0.168

0.96,0.24

1.02,0.305

1.04,0.352

1.07,0.359

1.1,0.361

1.25,0.341

1.5,0.295

2,0.274

2.5,0.24

3,0.25

4,0.25