An introduction is given to the research activity that is underway to enable the prediction of turbomachinery aeroelastic forced response. An effort is being made to assemble a computer program (FREPS) which incorporates the aeroelastic structural models, unsteady aerodynamic models, and forcing function models. The structural and aerodynamic models are currently well developed. The forcing function models are at a primitive level. A significant activity has begun to identify the forcing functions due to stator-rotor aerodynamic interaction.


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    Title :

    Aeroelastic forced response analysis of turbomachinery


    Contributors:


    Publication date :

    1988-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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