Indicial Response Function for Finite-Thickness Airfoils, A Semi-Empirical Approach

Publication: Research - peer-reviewArticle in proceedings – Annual report year: 2011

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Original languageEnglish
TitlePapers
PublisherAmerican Institute of Aeronautics and Astronautics
Publication date2011
PagesAIAA 2011-542
StatePublished

Conference

Conference49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Number49
CountryUnited States
CityOrlando, FL
Period04-01-1107-01-11
Internet addresshttps://www.aiaa.org/ProceedingsDetail.aspx?id=3778

Keywords

  • Aeroelastic design methods

ID: 6226897