Wind tunnel simulation tests are reported that utilize a 20 inch powered nacelle for airframe integration studies. Considered are: effects of boattail positioning, nacelle size, aft fuselage drag, over-the-wing half span model installation, and turboprop and ducted fan configurations.


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    Title :

    Propulsion airframe integration


    Contributors:


    Publication date :

    1975-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





    Transonic Airframe Propulsion Integration

    R. E. Coltrin / B. W. Sanders / D. P. Bencze | NTIS | 1992


    Transonic airframe propulsion integration

    Coltrin, Robert E. / Sanders, Bobby W. / Bencze, Daniel P. | NTRS | 1992