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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    Titel :

    Study of Aerodynamic Technology for VSTOL Fighter/Attack Aircraft, Volume 1


    Beteiligte:
    J. R. Lummus (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    264 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    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