Effect of variations and directions and velocity of current on wind tunnel tests; case of rotating wings.


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    Title :

    Report from German Aeronautical Experiment Station of Adlershof, near Berlin, presenting theoretical mathematical discussion of method of determining distribution of lift on airplane wings in slightly non-homogeneous air current, based on Prandtl equations


    Additional title:

    Auftriebsverteilung und daraus abgeleitete Groessen fuer Tragfluegel in schwach inhomogenen Stromungen


    Contributors:
    Bausch, K. (author)

    Published in:

    Publication date :

    1939


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :