By use of theoretical treatment indicated by PRANDTL, it has been possible to generalize available experimental results so that predictions can be made of important wake parameters in terms of distance behind airfoil trailing edge and profile drag coefficient; method of application of theory to design of airplane is demonstrated.


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    Title :

    Downwash and wake behind plain and flapped airfoils


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1939


    Size :

    28 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :