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Air Resonance of Bearingless Rotor Helicopter with Elastomeric Damper in Forward Flight

2017; American Institute of Aeronautics and Astronautics; Volume: 54; Issue: 6 Linguagem: Inglês

10.2514/1.c034388

1533-3868

Junhao Zhang, Pinqi Xia,

Aerospace Engineering and Control Systems

No AccessEngineering NoteAir Resonance of Bearingless Rotor Helicopter with Elastomeric Damper in Forward FlightJunhao Zhang and Pinqi XiaJunhao ZhangNanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of China and Pinqi XiaNanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of ChinaPublished Online:26 Jun 2017https://doi.org/10.2514/1.C034388SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Friedmann P. P. and Hodges D. H., "Rotary Wing Aeroelasticity—A Historical Perspective," Journal of Aircraft, Vol. 40, No. 6, 2003, pp. 1019–1046. doi:https://doi.org/10.2514/2.7216 LinkGoogle Scholar[2] Weller W. H. and Peterson R. 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All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0021-8669 (print) or 1533-3868 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAircraft Components and StructureAircraft DesignAircraft Operations and TechnologyAircraftsAlgorithms and Data StructuresComputing and InformaticsComputing, Information, and CommunicationData ScienceEvolutionary AlgorithmHelicoptersRotorcraftsSignal Processing KeywordsRotor SystemsFuselagesFinite Element MethodSelf Excited VibrationTransient ResponsePerturbation MethodRotor BladesParticle Swarm OptimizationFrequency DomainIterative AlgorithmAcknowledgmentThis study has been supported by the Natural Science Foundation of China (Grant 11572150).PDF Received24 January 2017Accepted9 April 2017Published online26 June 2017