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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    Title :

    Study of aerodynamic technology for single-cruise engine V/STOL fighter/attack aircraft


    Contributors:

    Publication date :

    1982-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :