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- W2375644404 abstract "In this paper,experimental study(Ma=2.0 of cold flow) on a scramjet combustor model without combustion was carried on direct-connected facility.The effects of inflow parameter,length of isolator and back pressure on combustor and isolator flow field were analyzed and compared.The flow field of combustor was simulated with CFD software and the experimental results were compared.The results show that isolator configuration maximum back pressure capability is improved by length increase of the isolator,the combustor and isolator field becomes uniformity with decease of the blockage ratio in combustor's exit." @default.
- W2375644404 created "2016-06-24" @default.
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- W2375644404 date "2008-01-01" @default.
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- W2375644404 title "Study of the Scramjet Combustor Experiment" @default.
- W2375644404 hasPublicationYear "2008" @default.
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