航天推进技术研究院主办
Zhang Mengzheng,Zhang Zhongli,Ge Lihu,et al.Primary calculating model for integrated scramjet engine design[J].Journal of Rocket Propulsion,2005,31(01):14-20.
一体化超燃冲压发动机初步设计计算模型
- Title:
- Primary calculating model for integrated scramjet engine design
- 分类号:
- V430
- 文献标志码:
- A
- 摘要:
- 以总压恢复系数最大为目标,采用等激波强度和等激波角设计方法建立进气道模型;采用Ikawa“面积扩张因子”建立燃烧室模型;依据Edward方法初估尾喷管型面。在此基础上建立了一体化超燃冲压发动机进气道、隔离段、燃烧室及尾喷管计算模型,并对一体化设计的超燃冲压发动机模型进行了初步计算。
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