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- W2390278610 abstract "Hydrocarbon fuel ignition experiments were performed on directly connected pulse combustion facility.The test inflow parameters included stagnation temperature of 935 K and the Mach number of 4 at the entrance of isolator.Gaseous ethylene was ignited successfully and combustion was maintained stable by employing three combination assistant ignition methods: torch igniter combined with pilot hydrogen,self-combustion of pilot hydrogen and air throttle combined with pilot hydrogen.The experimental results indicate that when employing self-combustion of pilot hydrogen,the mass flow rate of hydrogen should be ranged from 0.43~12.61 g/s,and higher mass flow rate of hydrogen isn't helpful to ignition;for air throttle combined with pilot hydrogen ignition method,the injection pressure of hydrogen should be set at 5 MPa,and the throttle mass flow rate should be 10%~30% of inflow mass flow rate.At last the lean blow-out limit and rich operation limit of scramjet were researched with ethylene injected from upstream of cavity or cavity floor.The results show that two injection schemes have similar lean blow-out limits at equivalence ratio of 0.077,and the rich operation limits varies a lot at equivalence ratios of 0.327 and 0.471 respectively." @default.
- W2390278610 created "2016-06-24" @default.
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- W2390278610 date "2013-01-01" @default.
- W2390278610 modified "2023-09-23" @default.
- W2390278610 title "Experiments on hydrocarbon fuel ignition for scramjet at Mach 4" @default.
- W2390278610 hasPublicationYear "2013" @default.
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