An assessment was made of the aerodynamic uncertainties associated with the design of a cold-deck-environment Navy VSTOL fighter/attack aircraft utilizing jet-diffuser ejectors for vertical lift and vectored-engine-over-wing blowing for supercirculation benefits. The critical aerodynamic uncertainties were determined as those associated with the constraints which size the aircraft to a specified set of requirements. A wind tunnel model and test programs are recommended for resolving these uncertainties.


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    Title :

    Study of aerodynamic technology for VSTOL fighter/attack aircraft, volume 1


    Contributors:

    Publication date :

    1978-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :