Influence of aircraft and installation characteristics on design of propellers in 500 to 1000 shp class is shown; these characteristics have significant effect on propeller performance, weight, and stress levels; effects of aircraft geometry and flight conditions on propeller blade selection and pitch change system design are considered; selection of propeller blade is based on desired propeller performance, propeller diameter limitation, and steady and vibratory stress levels; magnitude of steady stress depends upon power loading of blade; magnitude of vibratory stress depends upon nacelle tilt, gross weight, lift characteristics and other aircraft parameters; examples of installations.


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    Title :

    Propeller design consideration for turbine powered aircraft


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1968 Propellers



    Publication date :

    1968


    Size :

    10 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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