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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    Title :

    Gulfstream II aerodynamic design


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

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



    Publication date :

    1967


    Size :

    10 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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