Two powered-lift concepts, the tandem fan and the longitudinally-arrayed ejector, are integrated with two existing fighter aircraft, the F-14A and F-16A respectively, to indicate the benefits and/or penalties involved with providing STOVL capability to CTOL aircraft. It is shown that properly designed powered-lift aircraft can achieve either comparable or superior mission performance relative to CTOL aircraft.


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    Titel :

    Supersonic STOVL research aircraft


    Beteiligte:
    Wilson, S. B., III (Autor:in) / Kidwell, G. H., Jr. (Autor:in) / Turney, G. E. (Autor:in) / Rogers, A. (Autor:in)

    Erscheinungsdatum :

    01.10.1982


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Supersonic STOVL Research Aircraft

    Rogers, Al / Turney, George E. / Kidwell, George H. et al. | SAE Technical Papers | 1982


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