The NASA Lewis aeroelastic research program is focused on unstalled and stalled flutter, forced response, and whirl flutter of turborotors and propfans. The objectives are to understand the physical phenomena of cascade flutter and response including blade mistuning.


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    Title :

    Development of Aeroelastic Analysis Methods for Turborotors and Propfans, Including Mistuning


    Contributors:

    Publication date :

    1988


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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