The renewed interest in high-speed propulsion has led to increased activity in the development of the supersonic combustion ramjet engine for hypersonic flight applications. In the hypersonic regime the scramjet engine's specific thrust exceeds that of other propulsion systems. This book, written by a leading researcher, describes the processes and characteristics of the scramjet engine in a unified manner, reviewing both theoretical and experimental research. The focus is on the phenomena that dictate the thermo-aerodynamic processes encountered in the scramjet engine, including component analyses and flowpath considerations; fundamental theoretical topics related to internal flow with chemical reactions and non-equilibrium effects, high-temperature gas dynamics, and hypersonic effects are included. Cycle and component analyses are further described, followed by flowpath examination. Finally, the book reviews experimental and theoretical capabilities and describes ground testing facilities and computational fluid dynamics facilities developed for the study of time-accurate, high-temperature aerodynamics.


    Zugriff

    Download

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The Scramjet Engine : Processes and Characteristics


    Beteiligte:
    Segal, Corin (Autor:in)


    Ausgabe :

    Online-Ausg.


    Erscheinungsdatum :

    2011


    Format / Umfang :

    Online-Ressource (1 online resource (270 p.))


    Anmerkungen:

    digital, PDF file(s).
    Campusweiter Zugriff (Universität Hannover) - Vervielfältigungen (z.B. Kopien, Downloads) sind nur von einzelnen Kapiteln oder Seiten und nur zum eigenen wissenschaftlichen Gebrauch erlaubt. Keine Weitergabe an Dritte. Kein systematisches Downloaden durch Robots
    Title from publishers bibliographic system (viewed on 18 Feb 2013)




    Medientyp :

    Buch


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Klassifikation :

    BKL:    50.34 Gasdynamik, Aerodynamik / 52.30 Strömungskraftmaschinen, Turbomaschinen
    RVK:    ZO 7270
    DDC:    629.134/353







    Analysis of Scramjet Engine Characteristics

    T. Kanda / G. Masuya / Y. Wakamatsu et al. | NTIS | 1989