The paper proposes the technique based on solutions of the Reynolds-averaged Navier–Stokes (RANS) equations for selecting the optimal aerodynamic configuration of the wing at the early design stages. The general optimization algorithm is presented taking into account a great number of design variables and constraints. A parameterization approach is presented that allows the efficient manipulation of the wing geometry. The results of aerodynamic optimization of the isolated wing of the second-generation supersonic passenger aircraft are presented.


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    Titel :

    Optimization of the Aerodynamic Configuration of the Isolated Wing for the Second-Generation Supersonic Passenger Aircraft


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:

    Erschienen in:

    Russian Aeronautics ; 67 , 1 ; 70-79


    Erscheinungsdatum :

    2024-03-01


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch








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