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Flight Thrust, Power, and Energy Relations
Figure 1: Drag polar and drag polar components for electric sport aircraft. AR = 9.0 0 2 4 6 8 10 0 2 4 6 8 10 12 14 Pprop [W] V [m/s] Figure 2: Propulsive thrust power Pprop = DV = TV for electric sport aircraft. The corresponding propulsive power is shown in Figure 2. Minimum Flight Energy for Given Payload
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