It is recalled that for a detailed propeller design, theoretical models have to be used which are now available to the designer in computer programs. A brief review of the assumptions, on which various propeller models are based, is given. A procedure in use at the NSMB, for the evaluation of the pressure distribution on the blade sections of a propeller in off-design conditions, is discussed.


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    Title :

    Derivation of propeller blade section properties from lifting surface theory1


    Contributors:

    Published in:

    Publication date :

    1980-10-01


    Size :

    11 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English