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- W2335444490 abstract "Two series tests were conducted on the hydrocarbon fueled direct-connect scramjet test facility to optimize the configuration and fuel injection distribution, and to investigate their effects on scramjet combustor performances. The optimal configuration and fuel injection obtained in Test A improved performances with pedestal force increment, inner-force and synthesis Isp of optimal configuration increasing of 11.3%, 6.4% and 7.5% respectively compared with baseline configuration. Test B had a circumferential fuel injection distribution, and the test results showed a better combustor performance can be obtained. Fuel injection distribution closing entrance and concentrating appropriately will help to obtain best combustor performance; and a proper circumferential fuel distribution will lead better combustor performance. The coupled effects of configuration and fuel injection distribution on combustor performance are stronger than that of individual factors, and equivalence ratio is a dominant factor to pedestal force increment and combustor innerforce. In addition, the inner-force synthesis specific impulse was defined to enhance the comparability of combustor performances at flight condition." @default.
- W2335444490 created "2016-06-24" @default.
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- W2335444490 date "2007-07-08" @default.
- W2335444490 modified "2023-09-27" @default.
- W2335444490 title "Effects of the Configuration and Fuel Injection on Scramjet Combustor Performance" @default.
- W2335444490 cites W2153940033 @default.
- W2335444490 doi "https://doi.org/10.2514/6.2007-5421" @default.
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