Open Access

Table 6

Co-efficient of lift (Cl) of NACA 0012 with varying angle of attack (α) at velocity 8.1 m/s.

Angle of attack, α (degree) Coefficient of lift, Cl
–15 –1.425
–10 –1.1050
–5 –0.482
0 0.131
5 0.508
10 1.060
15 1.445
20 0.954

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