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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    Titel :

    Derivation of propeller blade section properties from lifting surface theory1


    Beteiligte:
    van Gent, W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.10.1980


    Format / Umfang :

    11 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Schlagwörter :





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