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高超声速发动机不同燃烧模式的性能比较──斜爆轰发动机性能评价
袁生学; 黄志澄
Source Publication空气动力学学报
1995
Volume13Issue:1Pages:48-56
ISSN0258-1825
Abstract本文采用热力学分析方法，从熵和的概念出发，论证了理想情况下爆轰发动机的有效性，并定量比较了在同样入口压缩条件下，采用爆轰、等压、等Ｍ数等三种燃烧模式的发动机的性能，证明Ｃ─Ｊ斜爆轰是最佳超声速燃烧模式。
Keyword斜爆轰波 超声速燃烧 吸气式发动机 热力循环
Language中文
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/35178
Collection力学所知识产出(1956-2008)
Corresponding Author袁生学
Recommended Citation
GB/T 7714		 袁生学,黄志澄. 高超声速发动机不同燃烧模式的性能比较──斜爆轰发动机性能评价[J]. 空气动力学学报,1995,13,1,:48-56.
APA 袁生学,&黄志澄.(1995).高超声速发动机不同燃烧模式的性能比较──斜爆轰发动机性能评价.空气动力学学报,13(1),48-56.
MLA 袁生学,et al."高超声速发动机不同燃烧模式的性能比较──斜爆轰发动机性能评价".空气动力学学报 13.1(1995):48-56.
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