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The mixing and combustion enhancement mechanisms induced by the coupling of cavity and shock were revealed. The numerical results indicated that autoignition dominated the combustion, while flame propagation mainly occurred near flame boundaries and fuel nozzle.
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This page is a summary of: Investigation of Mixing and Combustion Characteristics in a Mach 8 Circular Scramjet Combustor, AIAA Journal, July 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j065087.
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