A computational procedure is developed, based on lifting line theory, which successfully predicts the spanwise lift distribution at moderate blowing momentum coefficient on a high aspect ratio (AR = 18) circulation control wing-body model with several variations in the spanwise lift distribution which validates this procedure. Additional keywords: Coanda surface; Wing body configurations; Mathematical models. (Author)


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    Titel :

    Lift Distribution on a High Aspect Ratio Circulation Control Wing with Root Lift Cutout


    Beteiligte:
    R. J. Furey (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    53 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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