Rotorcraft Design for Maximized Performance at Minimized Vibratory Loads

    Research output: Chapter in Book/Conference proceedings/Edited volumeChapterScientific

    Original languageEnglish
    Title of host publicationAeronautics and Astronautics
    EditorsM Mulder
    Place of PublicationCroatia
    PublisherIntechOpen
    Pages237-256
    Number of pages610
    ISBN (Print)978-953-307-473-3
    DOIs
    Publication statusPublished - 2011

    Keywords

    • Boekdeel internat.wet

    Cite this

    Pavel, MD. (2011). Rotorcraft Design for Maximized Performance at Minimized Vibratory Loads. In M. Mulder (Ed.), Aeronautics and Astronautics (pp. 237-256). IntechOpen. https://doi.org/10.5772/25235