Abstract Hypersonic propulsion has been subjected to an intense research for the future propulsion. Various techniques have been proposed to replace the existing techniques. Most of them are chemical propulsion system, in which combustion plays a vital role in heat addition and its conversion to kinetic energy. The Ram Accelerator [1, 2], (referred to as RamAc), a ramjet-in-tube concept, is a propulsion concept based on using the Shock-Induced Combustion (SIC) to accelerate the projectile to a very high velocity. In a Ram accelerator, a projectile travels at supersonic speed in a launch tube, filled with a premixed fuel-oxidizer mixture


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    Titel :

    Numerical Simulation of Super-Detonative Ram Accelerator; Its Shock-Induced Combustion and Oblique Detonation


    Beteiligte:


    Ausgabe :

    1st ed. 2016


    Erscheinungsdatum :

    01.01.2016


    Format / Umfang :

    51 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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