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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    Title :

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


    Contributors:
    R. J. Furey (author)

    Publication date :

    1985


    Size :

    53 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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