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- The characteristic of static pressure profiles in supersonic combustor was analyzed. 对超声速燃烧室内的静压分布特点作出了分析;
- The OH fluorescence image in the flame of supersonic combustor displays OH difference distribution at different time. 由超声速燃烧室的OH荧光测量,可以看出不同时间OH分布的差别。
- The scramjet supersonic combustor and its test facility have been designed by enthalpy method and characteristic line method. 采用热焓法、特征线法等进行了超音燃烧室试验器的计 算和设计工作。
- The most difficult problem in the design of scramjet is that, how to design an optimization configuration of supersonic combustor. 超燃冲压发动机设计技术中的难点之一是超音速燃烧室结构设计。
- The OH fluorescence imaging is obtained in flames of flat flame burner, atom gasifier and supersonic combustor by planar laser induced fluorescence(PLIF)using single laser pulse. 用平面激光诱导荧光技术测量了平面火焰炉、原子气化炉和超声速燃烧室的单脉冲激光诱导OH荧光。
- The results of calculation show that the flameholding range of supersonic combustor can be enlarged using cavity and the combustion efficiency is improved. 计算结果表明,空腔扩大了超燃燃烧室的火焰稳定工作范围,并提高了燃烧效率。
- An experimental study of cold flow field was conducted under entrance Mach number 2.5 on a supersonic combustor experiment rig with subsonic pilot combustor and stream wise vortices mixer. 摘要结合对应的数值计算,对一种带亚声速预燃室和流向涡掺混器的超声速燃烧模型燃烧室实验台,在其进口马赫数为2.;5的来流条件下,进行了冷态流场的实验研究。
- A one-dimensional numerical analysis of supersonic combustor performance 超声速燃烧室性能一维数值模拟
- Analysis and application of gas sampling in the direct-connect supersonic combustor testing 直联式超燃实验台超声速燃气取样分析
- Experimental Investigation of Kerosene Ignition and Combustion in Supersonic Combustor 超音速燃烧室煤油强迫点火试验研究
- Investigation on selfignition characteristics of kerosene hydrogen dual fuel in supersonic Combustor 煤油-氢双燃料超声速燃烧点火特性研究
- The physics of supersonic flight. 超音速飞行的物理性质
- Have you taken supersonic aircraft? 你坐过超音速飞机吗?
- supersonic combustor 超声速燃烧室
- Developing the supersonic jet was quite an accomplishment. 开发超音速喷气机是一项了不起的成就。
- Full-Scalc Liquid Fuel Ramjet Combustor Tests. 全尺寸液体冲压发动机燃烧室试验。
- The Navy also needed a supersonic fighter. 海军也需要一架超音速战机。
- Fig. 2 Schematic of the combustor model. 图2微燃烧器数值模型内部结构。
- Supersonic Channel Airfoils for Reduced Drag. 减小阻力的超音速波道翼型。
- France Gauges Future Of Supersonic Transport. 法国评估超音速运输机的未来。