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. (English Abstract) (See also Luftfahrtforschung v 13 n 12 Dec 20 1936 p 405-9)


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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 :

    1937


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :