Load reduction potential using airfoils with variable trailing edge geometry

T. Buhl, M. Gaunaa, C. Bak

    Research output: Chapter in Book/Report/Conference proceedingArticle in proceedingsResearchpeer-review

    Original languageEnglish
    Title of host publication[Technical papers] presented at the 42. AIAA aerospace sciences meeting and exhibit
    Place of PublicationReston, VA
    PublisherAmerican Institute of Aeronautics and Astronautics
    Publication date2005
    Publication statusPublished - 2005
    Event43rd AIAA Aerospace Sciences Meeting and Exhibit - Grand Sierra Resort Hotel, Reno, NV, United States
    Duration: 10 Jan 200513 Jan 2005
    Conference number: 43

    Conference

    Conference43rd AIAA Aerospace Sciences Meeting and Exhibit
    Number43
    LocationGrand Sierra Resort Hotel
    CountryUnited States
    CityReno, NV
    Period10/01/200513/01/2005
    SeriesAIAA-2005-1183

    Cite this

    Buhl, T., Gaunaa, M., & Bak, C. (2005). Load reduction potential using airfoils with variable trailing edge geometry. In [Technical papers] presented at the 42. AIAA aerospace sciences meeting and exhibit American Institute of Aeronautics and Astronautics. AIAA-2005-1183