Approximate determination of lowest possible drag of airplanes of high aerodynamic efficiency; drag coefficient of streamlined bodies and of airfoils in super-critical range; permissible granulation of aerodynamically fully smooth surfaces; power calculation of airplanes on basis of plane friction. (See also in Aircraft Eng v 7 n 82 Dec 1935 p 318 and v 8 n 86 Apr 1936 p 103-8)


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    Title :

    Berechnung des Oberflacheureibungswiderstandes schneller Flugzeuge


    Additional title:

    Berechnung des Oberflacheureibungswiderstandes schneller Flugzeuge


    Contributors:
    Hoerner, S. (author)

    Published in:

    Publication date :

    1935


    Size :

    5 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German