An indirect method for finding shock-free airfoils and a nearly direct method for finding shock-free airfoils and wing are discussed. While the mathematics of both procedures is emphasized, illustrative practical results are given. (Author)


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    Titel :

    Shock-Free Configurations in Two- and Three- Dimensional Transonic Flow


    Beteiligte:
    A. R. Seebass (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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