A procedure that allows rapid preliminary evaluations of the vertical, short, and normal takeoff performance of supersonic cruise aircraft concepts was developed into a numerical computer program. The program is used to determine the effects on takeoff performance of various parameters, such as thrust-weight ratio, wing loading, thrust vector angle, and flap setting. Ramp-assisted takeoffs for overloaded configurations typical of a ground-attack mission are included. The effects of wind on the takeoff performance are also considered.


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    Title :

    Calculation of Vertical and Ramp-Assisted Takeoffs for Supersonic Cruise Fighters


    Contributors:
    G. C. Liu (author)

    Publication date :

    1984


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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