Short takeoff vertical landing (STOVL) aircraft offer unique basing and operational advantages to improve the capabilities of military forces in future warfare. To develop a STOVL fighter design with supersonic capability requires the integration of an advanced propulsion system into the airframe design. A promising propulsion system for supersonic STOVL application is the relatively new Hybrid Fan Vectored Thrust (HFVT) concept. This advanced Tandem Fan concept incorporates a dual-cycle engine with front and rear fully vectorabie nozzles of the three-poster type, to provide the required performance. In this paper, the HFVT STOVL design integration approaches for a conceptual fighter/attack aircraft, as well as some features of the resulting design, will be presented.


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    Titel :

    Conceptual Design of a STOVL Fighter/Attack Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Chin, Y.T. (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1988



    Erscheinungsdatum :

    01.10.1988




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch