In an analysis of Figure 7 a, it can be seen that when the spacing ratio h/R is increased from 0.2 to 0.5, the rotor lift shows an increasing trend.
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Aerodynamic Analysis of Rotor Spacing and Attitude Transition in Tilt-Powered Coaxial Rotor UAV.
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The sentences
When the tilt angle increases from δ = 9° to δ = 13°, the velocity distribution at the blade shows a decreasing trend.