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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    Title :

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


    Contributors:
    R. R. Boyce (author) / T. McIntyre (author)

    Publication date :

    2010


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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