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- scramjet eombustor 火焰稳定器
- Hydrogen injection and scramjet ignition testing. 氢注入及冲压点火测试。
- Hypersonic propulsion test facility is important for the scramjet ground tests. 摘要高超声速推进风洞是进行超燃冲压发动机模型地面模拟的重要试验设备。
- The thermal environment of the scramjet strut leading edge is rigorous. 摘要在超燃冲压发动机工作过程中，支板前缘的热环境非常恶劣。
- As part of this effort, an integrated scramjet model is about to begin testing at up to Mach 5.6 in a new wind tunnel in Beijing. 作为该项工作的一部分，一个可达5.;6马赫的综合冲压模型即将在北京的一个新的风洞内开始测试。
- "The facility is to provide high enthalpy [thermal dynamic] model scramjet testing," he says. “该实验室将提供高焓值[热动力学]模型超燃冲压发动机测试，”他说。
- In this thesis, the scramjet nozzle has been designed and optimized by the method of characteristic line. 本文应用简易特征线方法对超燃冲压发动机尾喷管进行了优化设计。
- The core of airbreathing technology is scramjet and airframe/propulsion integrated hypersonic flight vehicle. 吸气式高超声速技术的核心是超燃冲压发动机技术和机体／推进一体化飞行器技术。
- Advanced ramjet technologies are also important for scramjet development, and the Chinese have been active in this area for decades. 先进亚燃冲压技术对于超燃冲压技术至关重要，而中国数十年来在这一领域一直很活跃。
- DONBAR J,POWELL O,GRUBER M,JACKSON T.Post-test analysis of flush-wall fuel injection experiments in a scramjet combustor[R].AIAA 2001-3197. 张鹏;俞刚.;超燃燃烧室一维流场分析模型研究[J]
- Configurations of sidewall and location of cowl have significant influence on the performance of sidewall-compression scramjet inlets. 摘要侧板构型和唇口位置是影响侧压式进气道性能的关键参数。
- The necessity about using supersonic combustion ramjet(scramjet)for the single stage to orb(?)t aerospace plane is demonstrated. 本文首先说明了单级入轨的空天飞机采用超声速燃烧冲压发动机的必要性。
- This paper summarized the latest domestic and foreign development status of scramjet engine and focused on the key technologies. 超燃冲压发动机技术是一项新型的、具有广阔发展前景的推进技术。
- 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 results indicate that, the flow field distortion of 2-D scramjet inlet was much weaker than that of the sidewall compression scramjet inlet. 二元进气道流量系数对飞行马赫数的敏感程度远高于侧压式进气道；
- Preliminary investigation for scramjet engine performed by Beijing Power Machineries Institute is described in this paper. 介绍了北京动力机械研究所进行的超燃冲压发动机初步研究。
- Scramjet ignition technology and work on cooling the internal walls of a scramjet are also being assessed, the Chinese say. 该中国人透露，超燃冲压发动机点火技术和冷却超燃冲压发动机内壁的工作也在评估之中。
- In this paper, experimental and computational methods were introduced to study the characters of scramjet nozzle and to guide the design. 为了解超燃冲压发动机的工作特性,并设计其合理的构型,本文采用试验和仿真两种方法对超燃冲压发动机尾喷管进行了研究。
- In the recent ten years, scramjet design, computational and experimental studies has been developed rapidly in the world. 近十年来国内外在超燃冲压发动机设计、数值模拟及试验研究方面发展迅速。
- The airframe and engine highly integration nature of hypersonic vehicle results in the asymmetry and cowl adjustable characters of the scramjet nozzle. 由于高超声速飞行器机体与发动机高度一体化的构型,使超燃冲压发动机尾喷管具有非对称,面罩可调等特点。
