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- W616047899 abstract "The predicted dynamic stability of the XV-15 tilting proprotor aircraft in cruise flight is updated, using a reduced increase in the pitch gimbal coupling with collective, and a higher nominal control system stiffness. The major influence of the pitch-lag coupling of the XV-15 gimballed, stiff-inplane rotor on the aircraft stability is shown. The influence of the blade pitch dynamics is found to be contained primarily in the quasistatic pitch-lag and pitch-gimbal coupling, although the complete dynamics is retained in the analysis for an accurate quantitative calculation of the stability boundary." @default.
- W616047899 created "2016-06-24" @default.
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- W616047899 date "1977-02-01" @default.
- W616047899 modified "2023-09-27" @default.
- W616047899 title "The influence of pitch-lag coupling on the predicted aeroelastic stability of the XV-15 tilting proprotor aircraft" @default.
- W616047899 hasPublicationYear "1977" @default.
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