Effects of bump parameters on hypersonic inlet starting performance
- Resource Type
- Original Paper
- Source
- Journal of Zhejiang University-SCIENCE A: Applied Physics & Engineering. 23(10):807-819
- Subject
Hypersonic inlet Bump Boundary layer flow Starting performance Large-scale separation bubble 高超声速飞行器 鼓包 边界层气流 起动性能 大尺度分离区 - Language
- English
- ISSN
- 1673-565X
1862-1775