This project has investigated the fundamental scaling laws for supersonic combustion in scramjets flying at Mach 8. Developing these laws is critical for successfully transitioning small-scale ground test and flight experiment data to the design of full-scale scramjet vehicles. To achieve this, the project has employed state-of-the-art diagnostics to investigate inlet- injection radical farming supersonic combustion in a shock tunnel over a wide range of dynamic pressures at flight Mach 8.


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    Titel :

    Combustion scaling laws and inlet starting for Mach 8 inlet-injection radical farming scramjets


    Beteiligte:
    R. R. Boyce (Autor:in) / T. McIntyre (Autor:in)

    Erscheinungsdatum :

    2010


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Boyce, R.R. / McIntyre, T. / Schloegel, F. et al. | British Library Conference Proceedings | 2011


    Inlet Starting of High-Contraction Axisymmetric Scramjets

    Ogawa, H. / Grainger, A. / Boyce, R. et al. | British Library Conference Proceedings | 2009



    Inlet Starting of High-Contraction Axisymmetric Scramjets

    Ogawa, Hideaki / Grainger, Alexander L. / Boyce, Russell R. | AIAA | 2010


    Inlet Starting of High-Contraction Axisymmetric Scramjets

    Ogawa, Hideaki / Grainger, Alex / Boyce, Russell | AIAA | 2009