The 'Prago-Figiaivsky' wing theory of small aspect ratio was generalized, and the formulae for the coefficients of normal force, induced resistance and the center of pressure were established. A method was suggested to evaluate the lower limit of the critical angle of attack. After having recalculated the hydrodynamic forces of a rectangular plate, this method was applied to the ship after rudder and propeller. The results are in satisfactory agreement with the known experimental and calculated results. (Author)


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    Titel :

    Low-Aspect-Ratio Wing Theory and Its Application to the Ship Rudder


    Beteiligte:
    L. Ying-chung (Autor:in) / S. Hung-tsui (Autor:in) / L. Heng-mou (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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