Transonic wind tunnel study of control span and large wing-tip nacelles results on effectiveness of spoiler-slot-deflector controls on fighter aircraft


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    Title :

    Transonic wind-tunnel investigation of the effect of control span and large wing-tip nacelles on effectiveness of spoiler-slot- deflector controls on an unswept-wing fighter-type airplane


    Contributors:

    Publication date :

    1960-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English