Previous report gave calculations for pressure distribution over thin oblique airfoils at supersonic speed; present report extends calculations to subsonic speeds; it is found that flows again can be obtained by superposition of elementary conical flow fields; in case of sweepback wing pressure distributions remain qualitatively similar at subsonic and supersonic speeds. See also Engineering Index 1946 p 23.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Subsonic flow over thin oblique airfoils at zero lift


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Jones, R.T. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    13 pages


    Anmerkungen:

    7 Supp Plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :