Control of Flow Separation on a Contour Bump by Jets: An Experimental Study
Abstract
The usage of three-dimensional contour bumps in shock control under transonic flows becomes an active research topic in the aerospace industry
- Publication:
-
29th International Symposium on Shock Waves 2
- Pub Date:
- 2015
- DOI:
- 10.1007/978-3-319-16838-8_98
- Bibcode:
- 2015shw2.conf.1399L
- Keywords:
-
- Physics