Gulfstream II business jet is low wing aircraft of moderate sweep featuring T-tail arrangement and two aft-mounted turbofan engines; aerodynamic development of configuration and control system; significant design and aerodynamic characteristics with appropriate experimental data including force, pressure, and flow visualization results; wing optimization to meet requirements of high and low speed performance and pitch-down stall break at all flight conditions while providing adequate fuel volume; nacellepylon-wing relationship for optimum drag, engine characteristics, and airplane balance; empennage arrangement providing satisfactory stability and control of all conceivable flight conditions.


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    Titel :

    Gulfstream II aerodynamic design


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Waaland, I.T. (Autor:in) / Curtis, E.J. (Autor:in)

    Kongress:

    SAE Meeting ; 1967 ; United States , Wichita, KS Jet propelled



    Erscheinungsdatum :

    1967


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Gulfstream II Aerodynamic Design

    Curtis, E. J. / Waaland, I. T. | SAE Technical Papers | 1967


    Computational aerodynamic design of the Gulfstream IV wing

    CHANDRASEKHARAN, R. M. / MURPHY, W. R. / TAVERNA, F. P. et al. | AIAA | 1985


    Computational aerodynamic design of the Gulfstream IV wing

    CHANDRASEKHARAN, R. / MURPHY, W. / TAVERNA, F. et al. | AIAA | 1985


    Gulfstream

    Online Contents | 2012


    Gulfstream

    Online Contents | 2012