Representation of lift for fairly general family of wing body configurations (with no afterbody) in linearized supersonic flow considered over entire range of parameters; bracketing limits of lift obtained simply, using most elementary considerations when interpretation of these limits is recognized.


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    Title :

    Supersonic wing-body lift


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1951


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :