Publikationsdatum:
2018-06-06
Beschreibung:
Methodology similar to that used for our closed-loop control of Separation over NACA 0012 Airfoil (Pinier et al, AIAA Journal 2007) Synthetic Jet Actuators, Miniature Pressure Transducers Split POD with and without Actuations Flow state estimation from Pressure signature
Schlagwort(e):
Aerodynamics
Materialart:
Minnowbrook VI: 2009 Workshop on Flow Physics and Control for Internal and External Aerodynamics; 509-529; NASA/CP-2010-216112
Format:
application/pdf