A study was conducted to demonstrate the ability of a low order panel aerodynamic flow code to predict the aircraft-induced propeller plane flow field and the resulting steady state propeller blade loads for a single-rotation, wing-mounted tractor system. Comparisons between predicted and measured flow field surveys and resulting blade loads, including the first five harmonics, were made for the U.S. Navy P-3C land-based patrol turboprop aircraft. The study showed that low order flow codes accurately model the induced flow field.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Application of a Panel Method (QUADPAN) to the Prediction of Propeller Blade Loads


    Additional title:

    Sae Technical Papers


    Contributors:
    Conner, F. (author) / Dupcak, J. D. (author) / Donham, R. E. (author)

    Conference:

    SAE Aerospace Technology Conference and Exposition ; 1986



    Publication date :

    1986-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    PROPELLER BLADE WITH CONTROL PANEL

    PFALLER RUPERT / EHNENKL BERNKHARD | European Patent Office | 2015

    Free access

    PROPELLER AND PROPELLER BLADE

    NYIRI ATTILA / CIRUS ROBERT / CIRUS NORBERT | European Patent Office | 2021

    Free access

    PROPELLER AND PROPELLER BLADE

    CÍRUS RÓBERT / NYÍRI ATTILA / CÍRUS NORBERT | European Patent Office | 2024

    Free access

    Propeller and propeller blade

    NYIRI ATTILA / CIRUS ROBERT / CIRUS NORBERT | European Patent Office | 2024

    Free access

    PROPELLER BLADE

    PICOT OLIVIER / AMAT PASCAL | European Patent Office | 2024

    Free access