Method of relating solution of flow field to solution of simpler or known boundary value problem is extended, subject to edge corrections for finite plan forms, to most general type of prescribed boundary conditions on wing in linearized potential field.


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    Title :

    Correspondence flows for wings in linearized potential fields at subsonic and supersonic speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1951


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :