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


    Size :

    264 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Study of aerodynamic technology for VSTOL fighter attack aircraft

    Burhans, W., Jr. / Crafta, V. J., Jr. / Dannenhoffer, N. et al. | NTRS | 1978



    Study of Aerodynamic Technology for VSTOL Fighter Attack Aircraft

    W. Burhans / V. J. Crafta / N. Dannenhoffer et al. | NTIS | 1978