A theoretical method of designing cambered slender wings to have low lift-dependent drag is described. The results of subsonic wind tunnel tests on a series of thin cambered delta wings of aspect ratio 2 are presented, and the significant drag reductions achieved are discussed in relation to theoretical predictions for the drag of cambered slender wings. (Author)


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    Titel :

    Low-Speed Wind-Tunnel Tests on the Lift-Dependent Drag of delta Wings with Conical Camber


    Beteiligte:

    Erscheinungsdatum :

    1974


    Format / Umfang :

    39 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Some simple conical camber shapes to produce low lift-dependent drag on a slender delta wing

    Brebner, G. G. / Großbritannien, Aeronautical Research Council | TIBKAT | 1959


    Delta Wings with Longitudinal Camber at Low Speed

    G. J. Hancock / R. K. Nangia | NTIS | 1970



    Slender Delta Wing with Conical Camber

    Rajendra K. Bera | AIAA | 1974