General relations needed for design of airfoils with arbitrary spanwise camber and having minimum induced drag for specified flight conditions are developed and relations for determining wing form necessary for maximum lift-drag ratio at cruise by optimizing wing with respect to profile and induced drag; sample calculations carried out for circular arc wing.


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    Titel :

    Aerodynamic design of wings with cambered span having minimum induced drag


    Weitere Titelangaben:

    NASA -- Tech Report


    Beteiligte:


    Erscheinungsdatum :

    1963


    Format / Umfang :

    63 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic design of wings with cambered span having minimum induced drag

    Cone, Jr., C.D. | Engineering Index Backfile | 1963



    Optimal Hyperelliptic Cambered Span Configurations for Minimum Drag

    Ranjan, Prateek / Ansell, Phillip J. / James, Kai A. | AIAA | 2019



    Correction: Optimal Hyperelliptic Cambered Span Configurations for Minimum Drag

    Ranjan, Prateek / Ansell, Phillip J. / James, Kai A. | AIAA | 2021