Effect of Angle of Attack on Vortex Asymmetry of Supersonic Flow Past a Conical Forebody
AIAA AVIATION FORUM AND ASCEND 2024
01.01.2024
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
2010-4838 Flow Asymmetry over a Conical Forebody Under Plasma Actuation
British Library Conference Proceedings | 2010
|