Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Analysis and Design of a Hypersonic Scramjet Engine with a Transition Mach Number of 4.00



    Kongress:

    47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2009 ; Orlando, FL



    Erscheinungsdatum :

    01.01.2009


    Format / Umfang :

    29 pages


    Anmerkungen:

    Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Design of Hypersonic Scramjet Engine Operating between Mach 5 to Mach 9

    Khan, Daniyal Ahmed / Hassan, M. Hammad / Qamar, Ihtzaz | IEEE | 2019


    High Mach Number Operation of Accelerator Scramjet Engine

    Curran, Damian / Wheatley, Vincent / Smart, Michael | AIAA | 2023


    An innovative thermal management system for a Mach 4 to Mach 8 hypersonic scramjet engine

    Chen, Felix / Tam, William / Shimp, Nancy et al. | AIAA | 1998


    Correction: High Mach Number Operation of Accelerator Scramjet Engine

    Curran, Damian / Wheatley, Vincent / Smart, Michael | AIAA | 2023