Experimental/theoretical correlations are presented which show that significant levels of leading-edge thrust are possible at supersonic speeds for certain planforms having the geometry to support the theoretical thrust-distribution potential. The new analytical process employed provides not only the level of leading-edge thrust attainable but also the spanwise distribution of both it and that component of full theoretical thrust which acts as vortex lift. Significantly improved aerodynamic performance in the moderate supersonic speed regime is indicated.


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    Titel :

    Supersonic wings with significant leading-edge thrust at cruise


    Beteiligte:
    Robins, A. W. (Autor:in) / Carlson, H. W. (Autor:in) / Mack, R. J. (Autor:in)

    Erscheinungsdatum :

    1980-04-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Supersonic wings with significant leading-edge thrust at cruise

    Robins, A. W. / Carlson, H. W. / Mack, R. J. | NTRS | 1980


    Supersonic wings with significant leading-edge thrust at cruise

    Robins, A. Warner / Carlson, Harry W. / Mack, Robert J. | TIBKAT | 1980


    Supersonic Wings with Significant Leading-Edge Thrust at Cruise

    A. W. Robins / H. W. Carlson / R. J. Mack | NTIS | 1980