A concept to obtain shock-free transonic flow for design aerodynamics of aircraft and turbomachinery is outlined. The method of elliptic continuation or method of fictitious gas represents a starting point for operational computational procedures to obtain supercritical airfoils and wings. Design examples illustrate the value of shock-free configurations for aerodynamic efficiency enhancement. The application of supercritical flow in aerodynamic concepts is mentioned.


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    Titel :

    Methods for Design Aerodynamics of Modern Transport Aircraft


    Beteiligte:
    H. Sobieczky (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    74 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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