Modeling of Laminated Reinforced Composite with Carbon Nanotube Interlayers to Estimate Structural Damping in a Rotorcraft Blade
AIAA Scitech 2019 Forum
01.01.2019
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Rotorcraft Blade Lag Damping Using Highly Distributed Tuned Vibration Absorbers
British Library Conference Proceedings | 1998
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