A pair of numerical methods for predicting the flow past hypersonic vehicle configurations that include wings, fins, flaps, and a propulsion system, are described. The governing equations and fundamental details of the solution methods are reviewed. Results for both geometrically simple test cases and realistic hypersonic configurations are given. Since there is still a considerable lack of experience for hypersonic flow calculations, extensive testing and verification are essential. This verification is done by comparison of results with experimental data and other numerical methods. The results presented prove that the methods used are robust, flexible, and accurate enough to fulfill the needs of the design process.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Numerical Methods for Aerothermodynamic Design of Hypersonic Space Transport Vehicles


    Beteiligte:
    K. M. Wanie (Autor:in) / A. Brenneis (Autor:in) / A. Eberle (Autor:in) / S. Heiss (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Numerical methods for aerothermodynamic design of hypersonic space transport vehicles

    Hubschrauber und Flugzeuge, Messerschmitt-Bölkow-Blohm GmbH, Ottobrunn | TIBKAT | 1992


    Aerothermodynamic Design Optimization of Hypersonic Vehicles

    Eyi, Sinan / Hanquist, Kyle M. / Boyd, Iain D. | AIAA | 2019


    Aerothermodynamic Design Optimization of Hypersonic Vehicles

    Eyi, Sinan / Hanquist, Kyle M. / Boyd, Iain D. | AIAA | 2018



    Constrained Aerothermodynamic Design of Hypersonic Vehicles

    Gally, Thomas / Campbell, Richard | AIAA | 2002