Investigation on flame characteristics approaching thermal chocking in a cavity-based supersonic combustor
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DOI: 10.1177/09544100221107248
Abstract: This study experimentally investigated the combustion process in a cavity-based supersonic combustor at the inflow condition of Mach 2.92 with stagnation pressure 2.6 MPa and stagnation temperature 1530 K. Time-averaged flame distribution and oscillation characteristics… read more here.
Keywords: cavity; injection; flame; combustor ... See more keywords