Rotor performance enhancement via localized pitch control and its effects on hub vibrations and pitch link loads

Author:

Küfmann Philip,Bartels Rainer,van der Wall Berend G.

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference49 articles.

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2. Johnson, W.: Helicopter Theory. Princeton University Press, Princeton (1980)

3. Stewart, W.: Second harmonic control on the helicopter rotor. J. R. Aeronaut. Soc. 2997(2472), 1–15 (1952)

4. Arcidiacono, P.J.: Theoretical performance of helicopters having second and higher harmonic feathering control. J. Am. Helicopter Soc. 6(2), 8–19 (1961)

5. Nguyen, K.Q.: Active suppression of stall on helicopter rotors by Army/NASA Rotorcraft Division. In: Proceedings of the 25th European Rotorcraft Forum, pp. C13-1–C13-8 (1999)

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