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- W1515975263 abstract "A theoretical approach is presented with the object of determining the natural frequencies and hub characteristics of a single‐rotor helicopter in free ground vibration for use in the analysis of self‐excited mechanical oscillations of hinged rotor blades. The method is intended to obviate the experimental determination of these parameters, a technique which necessitates the construction of the helicopter before its vibrational features can be explored." @default.
- W1515975263 created "2016-06-24" @default.
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- W1515975263 date "1952-12-01" @default.
- W1515975263 modified "2023-09-25" @default.
- W1515975263 title "The Helicopter in Free Ground Vibration" @default.
- W1515975263 doi "https://doi.org/10.1108/eb032235" @default.
- W1515975263 hasPublicationYear "1952" @default.
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