Magnetostrictively actuated control flaps for vibration reduction in helicopter rotors -- design considerations for implementation.
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Publication:5952783
DOI10.1016/S0895-7177(00)00307-1zbMath1198.93137OpenAlexW2007186279MaRDI QIDQ5952783
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Publication date: 22 January 2002
Published in: Mathematical and Computer Modelling (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/s0895-7177(00)00307-1
active control of vibrationsactive materials and structuresvibration suppression in helicopter rotors
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