Study of the attainable flow topologies in a supersonic blunt trailing edge at various blowing ratios
54th AIAA Aerospace Sciences Meeting
01.01.2016
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2016
|Blunt Trailing Edge Cooling Effects at Supersonic Regime
AIAA | 2009
|Supersonic blowing circular rector trailing edge device and aircraft
Europäisches Patentamt | 2022
|