Effects of Cowl Lip Angle on Starting Performances for a Mixed-Compression Two-Dimensional Axisymmetric Hypersonic Inlet

The third quasi-uniform B-spline was adopted to design the cowl profiles with various cowl lip angles. Starting performances were simulated by the numerical method and the results showed that the starting processes for different cowls can be classified into two types. In the first type, the inlet st...

詳細記述

書誌詳細

出版年:	Applied Sciences
主要な著者:	Yunfan Zhou, Shangcheng Xu, Yi Wang
フォーマット:	論文
言語:	英語
出版事項:	MDPI AG 2022-07-01
主題:	hypersonic inlet cowl lip angle starting performance large-scale separation bubble
オンライン･アクセス:	https://www.mdpi.com/2076-3417/12/14/7127