Historically, the Burrill diagram has been used early in the propeller design process to estimate the inception of thrust loss due to cavitation. That data was based on a systematic series of propeller tested in a uniform inflow. This report develops an alternative set of curves based on five modern propeller designs to estimate thrust breakdown for both uniform inflow and for a range of non-uniformities.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Thrust Breakdown Characteristics of Conventional Propellers


    Beteiligte:
    S. D. Black (Autor:in)

    Erscheinungsdatum :

    2007


    Format / Umfang :

    51 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    THRUST RINGS, PROPELLERS AND METHODS

    SHARROW GREGORY CHARLES / SACKSTEDER ANTHONY D | Europäisches Patentamt | 2025

    Freier Zugriff

    Thrust deduction in contrarotating propellers

    Beveridge, J. | Tema Archiv | 1974


    Static thrust of airplane propellers

    Diehl, Walter S | NTRS | 1934


    Static thrust of airplane propellers

    Diehl, W.S. | Engineering Index Backfile | 1932


    Thrust pressures on screw propellers

    Engineering Index Backfile | 1925