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1. The Reduction of Rotorcraft Power and Vibration Using Optimally Controlled Active Gurney Flap

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Open Access

2. Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft

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Open Access

3. Calibration of a Four Degree of Freedom Stewart Platform Sensor Subject to Translational and Rotational Constraints

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Open Access