The hodograph, fictitious gas, inverse and numerical optimization approaches are discussed for transonic wing and airfoil design. It is suggested that if a general design method for complete wings is required neither the fictitious gas method nor the local residual-correction type of inverse approach are adequate. An inverse approach allowing global wing design as well as local design modifications is the best compromise, numerical optmization being too expensive.


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    Titel :

    Computational Procedures in Transonic Aerodynamic Design


    Beteiligte:
    J. W. Slooff (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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