Analysis indicates that for aerodynamic efficiency, wings designed for flight at supersonic speeds should be swept back at angle greater than Mach angle and angle of sweepback should be such that component of velocity normal to leading edge is less than critical speed of airfoil sections; principle may also be applied to wings designed for subsonic speeds near speed of sound.


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    Titel :

    Wing plan forms for high-speed flight


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


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


    Erscheinungsdatum :

    1946


    Format / Umfang :

    11 pages


    Anmerkungen:

    Supp Sheets, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Wing plan forms for high-speed flight

    Jones, Robert J | NTRS | 1947


    Wing plan forms for high-speed flight

    Jones, Robert T | NTRS | 1946


    Wing plan forms for high-speed flight

    Jones, Robert T. | TIBKAT | 1945


    Wing planforms for high-speed flight

    Jones, R. T. | NTRS | 1976


    How Delta-wing aids high-speed flight

    McLarren, R. | Engineering Index Backfile | 1949