International Journal of Aerospace Engineering / 2019 / Article / Fig 1

Research Article

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

Figure 1

Lift-offset helicopters using ABC™.
(a) XH-59A Technology Demonstrator [2]
(b) X2 Technology Demonstrator [2]
(c) S-97 Raider [3]

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