Relation of speed and pressure distribution of airfoil profile to angle of attack; with aid of these relations derived from potential theory, theory of airplane wing can be checked and confirmed; comparison with actual measurements show satisfactory agreement.


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    Title :

    Die Abhaengigkeit der Geschwindigkeits -- und Druckverteilung an einem Tragfluegelprofil von Anstellwinkel


    Additional title:

    Die Abhaengigkeit der Geschwindigkeits -- und Druckverteilung an einem Tragfluegelprofil von Anstellwinkel


    Contributors:
    Weinig, F. (author)

    Published in:

    Publication date :

    1933


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :