Report discusses use of coupled aerodynamic/ and acoustical computer codes to predict noise emitted by turbopropeller blades turning at supersonic tip speeds. To predict noise field, existing turboprop-noise computer code by Farassat modified to accept blade-pressure inputs from three-dimensional turbofan aerodynamical computer code by Denton.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Coupled Aerodynamic/Acoustical Predictions For Turboprops


    Contributors:

    Published in:

    Publication date :

    1988-05-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Tradewind turboprops

    Withee, W.W. | Engineering Index Backfile | 1955


    Pressurized Turboprops

    British Library Online Contents | 2001


    Düsseldorf bans turboprops

    Online Contents | 1996


    Single-Engine Turboprops

    British Library Online Contents | 2001


    Pistons/Non-Pressurized Turboprops

    British Library Online Contents | 2001