Integration design and analysis for curved conical forebody and three-dimensional inward turning inlet

被引：0
|
作者：
机构：
[1] Li, Yiqing
[2] Zhou, Xunhuang
[3] Zhu, Chengxiang
[4] You, Yancheng
来源：
| 2018年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 33期
关键词：
Compendex;
D O I：
10.13224/j.cnki.jasp.2018.01.011
中图分类号：
学科分类号：
摘要：
Angle of attack - Flow rate - Integration - Mass transfer
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