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Corrigendum to “Dynamical analysis of propeller rotors whirl flutter considering complex blade geometries and induced velocities” [Mech. Syst. Signal Process. 230 (2025) 112621] (Mechanical Systems and Signal Processing (2025) 230, (S088832702500322X), (10.1016/j.ymssp.2025.112621))

  • Zhihong Song
  • , Jie Hong
  • , Zhefu Yang*
  • , Yitao Cao
  • , Yanhong Ma
  • *Corresponding author for this work
  • Beihang University
  • AECC Hunan Aviation Powerplant Research Institute

Research output: Contribution to journalComment/debate

Abstract

The authors regret the incorrect citation details concerning reference [45], specifically the publication year and the DOI: [45] V. Muscarello and G. Quaranta, “Exploration of the Effects of Rotor Blade Twist on Whirl-Flutter Stability Boundaries,” J. Aircr. (2023) 1 – 16, https://doi.org/10.2514/1.C0.34564. The correct citation should be: [45] V. Muscarello, G. Quaranta, Exploration of the effects of rotor blade twist on whirl-flutter stability boundaries. J. Aircraft 61(2) (2024) 570–585. https://doi.org/10.2514/1.C037479. The authors would like to apologise for any inconvenience caused.

Original languageEnglish
Article number112922
JournalMechanical Systems and Signal Processing
Volume236
DOIs
StatePublished - 1 Aug 2025

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