The design and development of an in-draft wind tunnel test section which will be used to study the dynamic stall of airfoils oscillating in pitch is described. The hardware developed comprises a spanned airfoil between schleiren windows, a four bar linkage, flywheels, a drive system and a test section structure.


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    Titel :

    Development of Drive Mechanism for an Oscillating Airfoil


    Beteiligte:
    C. D. Sticht (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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