Identification of Flap Motion Parameters for Vibration Reduction in Helicopter Rotors with Multiple Active Trailing Edge Flaps

Article English OPEN
Dalli, Uğbreve;ur; Yüksel, Şcedilefaatdin;
(2011)
  • Publisher: IOS Press
  • Journal: Shock and Vibration (issn: 1070-9622, eissn: 1875-9203)
  • Related identifiers: doi: 10.3233/SAV-2010-0594
  • Subject: Physics | QC1-999

An active control method utilizing the multiple trailing edge flap configuration for rotorcraft vibration suppression and blade loads control is presented. A comprehensive model for rotor blade with active trailing edge flaps is used to calculate the vibration character... View more
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