Study made in Langley tank to determine lift, drag, and pitching-moment characteristics of three hydrofoils, two triangular and one rectangular; triangular hydrofoil with leading-edge sweep had better overall lift drag ratios; maximum lift-drag ratio obtained was 5.0; pertinence to use of hydrofoil as landing gear for waterbased aircraft.


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    Titel :

    Force investigation of three surface-piercing supercavitating hydrofoils with 45° negative dihedral


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Weinstein, I. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    44 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Leading edge flutter of supercavitating hydrofoils

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



    Optimal Geometry for 3D Supercavitating Hydrofoils

    Çelik, F. / Bal, Ş. / Arıkan, Y. | TIBKAT | 2014

    Freier Zugriff

    Leading-edge flutter of supercavitating hydrofoils

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