MUCH has been said earlier concerning the scale effect on drag. A few words must be added on the scale effect on lift near the stall, for it is here that ordinary small-scale wind tunnel tests may be very misleading. The curves of Fig. 9 show the maximum lift coefficient of two wing sections plotted against Reynolds number, and the difference of behaviour is at once apparent.


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    Titel :

    Aeronautical Progress 1930–1936


    Untertitel :

    A Review of Scientific Progress Given in the James Forrest Lecture


    Beteiligte:
    Relf, E.F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1936-07-01


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Aeronautical Progress 1930–1936

    Relf, E.F. | Emerald Group Publishing | 1936


    Aeronautical progress, 1914-1930

    Southwell, R.V. | Engineering Index Backfile | 1930


    Aeronautical progress, 1914-1930

    Southwell, R.V. | Engineering Index Backfile | 1930


    Aeronautical progress, 1914-1930

    Southwell, R.V. | Engineering Index Backfile | 1930


    Aeronautical progress, 1914-1930

    Southwell, R.V. | Engineering Index Backfile | 1930