The Langley 1/8-scale V/STOL model tunnel was used to qualitatively determine the flow fields associated with semi-span close coupled canard wing and strake wing models. Small helium filled bubbles were injected upstream of the models to make the flow visible. Photographs were taken over the angle-of-attack ranges of -10 deg to 40 deg.


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    Titel :

    Flow visualization study of close-coupled canard wing and strake wing configuration


    Beteiligte:
    Miner, D. D. (Autor:in) / Gloss, B. B. (Autor:in)

    Erscheinungsdatum :

    1975-03-03


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :