Study of the attainable flow topologies in a supersonic blunt trailing edge at various blowing ratios
54th AIAA Aerospace Sciences Meeting
2016-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2016
|Blunt Trailing Edge Cooling Effects at Supersonic Regime
AIAA | 2009
|Supersonic blowing circular rector trailing edge device and aircraft
European Patent Office | 2022
|