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国外磁流动力学能量旁路超燃冲压发动机发展概况——一种新型高速冲压发动机 被引量:2
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作者 刘敬华 童建忠 +1 位作者 邢君波 徐逸梅 《飞航导弹》 2003年第9期45-46,54,共3页
关键词 重复使用空间运输计划 磁流体动力学 高速冲压发动机 超燃冲压发动机 飞行器
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Progress in research on mixing techniques for transverse injection flow fields in supersonic crossflows 被引量:9
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作者 Wei HUANG Li YAN 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2013年第8期554-564,共11页
The transverse injection flow field has an important impact on the flowpath design of scramjet engines. At present a combination of the transverse injection scheme and any other flame holder has been widely employed i... The transverse injection flow field has an important impact on the flowpath design of scramjet engines. At present a combination of the transverse injection scheme and any other flame holder has been widely employed in hypersonic propulsion systems to promote the mixing process between the fuel and the supersonic freestream; combustion efficiency has been improved thereby, as well as engine thrust. Research on mixing techniques for the transverse injection flow field is summarized from four aspects, namely the jet-to-crossflow pressure ratio, the geometric configuration of the injection port, the number of injection ports, and the injection angle. In conclusion, urgent investigations of mixing techniques of the transverse injection flow field are pro- posed, especiaUy data mining in the quantitative analytical results for transverse injection flow field, based on results from multi-objective design optimization theory. 展开更多
关键词 Aerospace propulsion system Transverse injection MIXING Supersonic crossflow
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