Aerodynamic theory as applied to the design of supersonic missile configuration is discussed. Emphasis is placed on the study of aerodynamic interference parameters among the elemental low aspect ratio wing-body-tail combinations.


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    Title :

    Wing-Tail Interference Experiments at Supersonic Speeds


    Contributors:

    Publication date :

    1963


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English