Given here is a brief description of the Gottingen Wind Tunnel for the testing of aircraft models, preceded by a history of its development. Included are a number of diagrams illustrating, among other things, a sectional elevation of the wind tunnel, the pressure regulator, the entrance cone and method of supporting a model for simple drag tests, a three-component balance, and a propeller testing device, all of which are discussed in the text.


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    Titel :

    Gottingen Wind Tunnel for Testing Aircraft Models


    Beteiligte:
    Prandtl, L (Autor:in)

    Erscheinungsdatum :

    01.11.1920


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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