There are plans to use the supercritical wing on the next generation of commercial aircraft so as to economize on fuel consumption by reducing drag. Computer codes have served well in meeting the consequent demand for new wing sections. The possibility of replacing wind tunnel tests by computational fluid dynamics is discussed. Another approach to the supercritical wing is through shockless airfoils. A novel boundary value problem in the hodograph plane is studied that enables one to design a shockless airfoil so that its pressure distribution very nearly takes on data that are prescribed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Transonic flow theory of airfoils and wings


    Beteiligte:


    Erscheinungsdatum :

    1976-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Airfoils and Wings in Transonic Ground Effect

    Doig, Graham / Barber, Tracie / Leonardi, Eddie et al. | AIAA | 2008



    Transonic flow about airfoils

    Bauer, F. / Garabedian, P. / Jameson, A. et al. | NTRS | 1978


    Transonic Airfoils and Wings Design Using Inverse and Direct Methods

    Zhang, Mengmeng / Rizzi, Arthur W. / Nangia, R K. | AIAA | 2015