[PDF][PDF] 咽式进气道设计工况下性能初步分析
辜天来， 付磊， 张帅， 郑耀 - 航空动力学报, 2014 - researchgate.net
介绍了三维内收缩高超声速咽式进气道的设计方法, 开发了相应的设计程序. 在高度为30km,
设计马赫数为5 和攻角为0 工况下进行设计, 使用CFD 模拟技术, 对设计方法和程序进行了验证 …
设计马赫数为5 和攻角为0 工况下进行设计, 使用CFD 模拟技术, 对设计方法和程序进行了验证 …
Preliminary analysis of jaws inlet performance under design conditions
GU Tian-lai, FU Lei, Z Shuai, Z Yao - 航空动力学报, 2014 - jasp.com.cn
The design method of the three-dimensional inward turning hypersonic jaws inlet was
introduced. Corresponding design codes were developed. Thereafter, a CFD technology …
introduced. Corresponding design codes were developed. Thereafter, a CFD technology …