A conceptual design analysis is performed on a single engine V/STOL supersonic fighter/attack concept powered by a series flow tandem fan propulsion system. Forward and aft mounted fans have independent flow paths for V/STOL operation and series flow in high speed flight. Mission, combat and V/STOL performance is calculated. Detailed aerodynamic estimates are made and aerodynamic uncertainties associated with the configuration and estimation methods identified. A wind tunnel research program is developed to resolve principal uncertainties and establish a data base for the baseline configuration and parametric variations.


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    Titel :

    Study of Aerodynamic Technology for Single-Cruise Engine V/STOL Fighter/Attack Aircraft


    Beteiligte:
    H. H. Driggers (Autor:in) / S. A. Powers (Autor:in) / R. T. Roush (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    208 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch