Some of the single rotation propfan model wind tunnel aeroelastic findings from the experimental part of this research program are described. These findings include results for unstalled or classical flutter, blade response from separated flow excitations, and blade response from aerodynamic excitations at angled inflow conditions.


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    Titel :

    Propfan Model Wind Tunnel Aeroelastic Research Results


    Beteiligte:
    O. Mehmed (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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