Application of low drag-due-to-lift concept of linearized theory to the studies of twist and camber of isolated wing and wing-body configurations of supersonic aircraft


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    Title :

    SUPERSONIC AERODYNAMIC CHARACTERISTICS OF SOME SIMPLIFIED AND COMPLEX AIRCRAFT CONFIGURATIONS WHICH EMPLOY HIGHLY SWEPT TWISTED-AND-CAMBERED ARROW-WING PLANFORMS


    Contributors:

    Publication date :

    1963-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English