A leading-edge correction is obtained via the method of matched asymptotic expansions to the first-order linearized solution for the potential flow past a supercavitating flat-plate hydrofoil at zero cavitation number. The composite expansions for the pressure on the plate and the shape of the upper cavity are seen to compare well with the exact solution due to Rayleigh.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Leading-edge correction for the supercavitating flat-plate hydrofoil


    Contributors:
    Plotkin, A. (author)

    Published in:

    Publication date :

    1977


    Size :

    7 Seiten, 8 Bilder, 7 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Leading edge flutter of supercavitating hydrofoils

    Brennen, C. / Oey, K. / Bancock, C.D. | Tema Archive | 1979


    Leading-edge flutter of supercavitating hydrofoils

    Brennen, C. / Oey, K.T. | Tema Archive | 1980


    A new approach to high-aspect-ratio supercavitating hydrofoil

    Kida, T. / Miyai, Y. | Tema Archive | 1979