International Journal of Aerospace Engineering / 2018 / Article / Fig 7

Research Article

Experimental Analysis of a Small-Scale Rotor at Various Inflow Angles

Figure 7

Comparison of thrust and power coefficients for MAE 11x7 at 90° angle of attack: (a) Ω = 4000 rpm; (b) Ω = 5000 rpm.
(a)
(b)

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