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    Demonstration Of Supersonic Combustion In A Combustion Driven Shock-Tunnel 

    Joarder, Ratan (2011-01-17)
    For flights beyond Mach 6 ramjets are inefficient engines due to huge total pressure loss in the normal shock systems, combustion conditions that lose a large fraction of the available chemical energy due to dissociation ...

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    AuthorJoarder, Ratan (1)Subject
    Air Injection (1)
    Combustion - Numerical Simulations (1)Combustion-Driven Shock Tunnel (1)
    Heat Engineering (1)
    Hypersonic Cross-flow (1)Hypersonic Flow (1)Hypersonic Shock Tunnel HST2 (1)Jet Injection (1)Shock Tunnel (1)Supersonic Combustion (1)... View MoreDate Issued2011 (1)Has File(s)Yes (1)

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