International Journal of Aerospace Engineering / 2019 / Article / Fig 10

Research Article

Vibration and Performance Analyses Using Individual Blade Pitch Controls for Lift-Offset Rotors

Figure 10

IBC input conditions using a single harmonic input for maximum reduction in 3/rev hub vibratory load components.
(a) /1°/φ
(b) /2°/φ
(c) /1°/φ
(d) /2°/φ
(e) /1°/φ
(f) /2°/φ

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