The primary objective is to determine how an airplane configuration should be modeled to predict both longitudinal and lateral aerodynamic characteristics at high angles of attack. A generic fighter model, an F-16 and an F-18 configuration with leading edge flap deflection and an F-106B configuration were investigated. Furthermore, the F-16XL and X-29 configurations were examined. Some calculated results are given.


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    Title :

    Calculation of aerodynamic characteristics at high angles of attack for airplane configurations


    Contributors:

    Publication date :

    1987-02-24


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :