Report from German Aeronautical Research Laboratory of Adlershof, near Berlin, on mathematical theory of airplane wings of finite span with particular reference to short spans, taking account of finite kinetic energy imparted to air by element of wing; lift decrease for small spans; comparison with experimental results. (see also brief English abstract in Aircraft Eng v 9 n 97 Mar 1937 p 84)


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    Title :

    Beitrag zur Theorie des Tragfluegels endlicher, insbesondere Kleiner Spannweite


    Additional title:

    Beitrag zur Theorie des Tragfluegels endlicher, insbesondere Kleiner Spannweite


    Contributors:
    Weinig, F. (author)

    Published in:

    Publication date :

    1936


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :