Calculations are presented for the forces on a thin supersonic wing underneath which the air is heated. The analysis is limited principally to linearized theory but nonlinear effects are considered. It is shown that significant advantages to external heating would exist if the heat were added well below and ahead of the wing.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Two-Dimensional, Supersonic, Linearized Flow with Heat Addition


    Beteiligte:
    Lomax, Harvard (Autor:in)

    Erscheinungsdatum :

    1959-02-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Vorticity Distribution in Linearized Supersonic Flow

    Gopal, Vijay / Maddalena, Luca | AIAA | 2018


    Linearized characteristics method for supersonic flow past vibratingshells.

    PLATZER, M. F. / BRIX, C. W. / WEBSTER, K. A. | AIAA | 1973


    Heat addition to a supersonic flow

    Burson, W.C. | Tema Archiv | 1976



    Linearized supersonic aerofoil theory -- II

    Gunn, J.C. | Engineering Index Backfile | 1947