Simultaneous Vibration Reduction and Performance Improvement of Helicopter Rotor Using Individual Blade Pitch Control with Multiple Harmonic Inputs

Author:

Park Jae-SangORCID

Funder

Korea Research Institute for defense Technology Planning and advancement

National Research Foundation of Korea

Ministry of Science and ICT

Publisher

Springer Science and Business Media LLC

Reference19 articles.

1. Yu YH, Tung C, van der Wall BG, Pausder HJ, Burley C, Brooks T, Beaumier P, Delrieux Y, Mercker E, Pengel K (2002) The HART-II test: rotor wakes aeroacoustics with Higher-Harmonic pitch Control (HHC) inputs—the joint German/French/Dutch/US project. In: Proceedings of the 58th American Helicopter Society annual forum

2. Jacklin SA, Blaas A, Teves D, Kube R, Warmbrodt W (1994) Reduction of helicopter BVI noise, vibration, and power consumption through individual blade control. In: Proceedings of the 51st American Helicopter Society annual forum

3. Norman TR, Theodore C, Shinoda PM, Fuerst D, Arnold UTP, Makinen S, Lorber P, O’Neill J (2009) Full-scale wind tunnel test of a UH-60 individual blade control system for performance improvement and vibration, loads, and noise control. In: Proceedings of the 65th American Helicopter Society annual forum

4. Yeo H, Romander EA, Norman TR (2011) Investigation of rotor performance and loads of a UH-60A individual blade control system. J Am Helicopter Soc 56(4):1–18

5. Yeo H, Jain R, Jayaraman B (2016) Investigation of rotor vibratory loads of a UH-60A individual blade control system. J Am Helicopter Soc 61(3):1–16

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