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乘波前体构型设计与压缩性能分析
Alternative TitleWaverider configuration design and forebody compressibility analysis
刘嘉; 王发民
Source Publication工程力学
2003-12-30
Volume20Issue:6Pages:130-134
ISSN1000-4750
Abstract提出了用相交楔锥流场构造乘波构型飞行器前体的方法。该方法利用无粘相交楔锥流场生成具有两个压缩面的乘波前体,不仅兼具楔型流场和锥型流场构造乘波体的优点,而且充分发挥了高超声速飞行器前体的预压缩作用,为进气道的正常工作提供了条件。同时用数值模拟的方法研究了不同前体压缩角度组合的预压缩效果,并在压缩角优化的基础上进行了前体/进气道的一体化设计。
Keyword乘波体 相交楔锥 压缩性 一体化设计
Indexed ByCSCD
Language中文
CSCD IDCSCD:1170054
Citation statistics
Cited Times:7[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/41622
Collection力学所知识产出(1956-2008)
Corresponding Author刘嘉
Recommended Citation
GB/T 7714
刘嘉,王发民. 乘波前体构型设计与压缩性能分析[J]. 工程力学,2003,20(6):130-134
APA 刘嘉,&王发民.(2003).乘波前体构型设计与压缩性能分析.工程力学,20(6),130-134.
MLA 刘嘉,et al."乘波前体构型设计与压缩性能分析".工程力学 20.6(2003):130-134.
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