Removed due to plagiarism. The original was published as: Numerical Investigation of Inlet-Combustor Interactions for a Scramjet Hydrogen-Fueled Engine at a Flight Mach number of 8. Authors: Edder Rabadan and Bernhard Weigand 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 2012. Paper ID AIAA-2012-5926, DOI: 10.2514/6.2012-5926


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    Titel :

    Numerical Simulation on Hypersonic Combustion of Hydrogen-Fueled Scramjet Combustor with Parallel Strut Fuel Injection at a Flight Mach Number of 7


    Erschienen in:

    Applied Mechanics and Materials ; 766-767 ; 1044-1049


    Erscheinungsdatum :

    08.06.2015


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    NUMERICAL INVESTIGATIONS OF INLET-COMBUSTOR INTERACTIONS FOR A SCRAMJET HYDROGEN-FUELED ENGINE AT A MACH FLIGHT NUMBER OF 8

    Santana, E.R. / Weigand, B. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012



    Operating Process Investigation of Hydrogen-Fueled Scramjet with Strut Fuel Feed System

    Semenov, V. / Romankov, O. / International Society for Air Breathing Engines; United States Committee | British Library Conference Proceedings | 1997


    Liquid-Fueled Strut-Based Scramjet Combustor Design: A Computational Fluid Dynamics Approach

    Manna, P. / Behera, Ramesh / Chakraborty, Debasis | AIAA | 2008