Cite
HARVARD Citation
Gennaretti, M. et al. (2015). Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices. International journal of aerospace engineering. p. . [Online].
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Gennaretti, M. et al. (2015). Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices. International journal of aerospace engineering. p. . [Online].