THE wind tunnel, through the use of models, offers a convenient means of investigating the aerodynamic characteristics of various parts of the aeroplane, individually or as a unit, and results obtained in it are generally applicable, within the limits of engineering precision, for the purpose of estimating full-scale performance. It is believed that the results of control surface tests on models may be taken to represent full-scale conditions with approximately the same degree of precision.


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    Titel :

    Control by Conventional Ailerons


    Untertitel :

    Results of a Series of Wind-Tunnel Experiments Carried out by the U.S. Bureau of Standards


    Erschienen in:

    Erscheinungsdatum :

    1931-12-01


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch