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Aerodynamic shape optimization via control theory of helicopter rotor blades using a non-linear frequency domain approach

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Identiferoai:union.ndltd.org:mcgill.ca/oai:escholarship.mcgill.ca:4m90dz935
Date January 2008
CreatorsTatossian, Charles A.
PublisherMcGill University
Source SetsMcGill University
Languagehttp://id.loc.gov/vocabulary/iso639-2/eng
Detected LanguageEnglish
TypeThesis
RightsAll items in eScholarship@McGill are protected by copyright with all rights reserved unless otherwise indicated.
RelationProquest: AAIMR51477, Pid: 112586

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