Recent progress in the development of a general purpose unsteady aerodynamic and aeroelastic analysis capability for Advanced Turboprops will be reviewed. An application to a rotor with alternating forward and backward swept blades is described, which illustrates the general 'mistuning' capability of the method.


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    Title :

    Aeroelastic effects of alternate blade sweep on advanced propfan rotor


    Additional title:

    Aeroelastische Wirkung der Wechsel-Blattpfeilung an zukunftsweisenden Propellerturbinen-Drehfluegeln


    Contributors:

    Published in:

    ASME-Papers ; Dec ; 1-6


    Publication date :

    1987


    Size :

    6 Seiten, 10 Bilder, 5 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English