Experimental Study on Delayed Feedback Flow Control around a NACA0015 Airfoil Using PSJA (AIAA 2017-0487)
55th AIAA Aerospace Sciences Meeting 2017 ; 2017 ; Grapevine, Texas
01.01.2017
9 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Separation Control over a NACA0015 Airfoil Using Nanosecond Pulsed Plasma Actuator (AIAA 2017-0715)
British Library Conference Proceedings | 2017
|POD Based Separation Control on the NACA0015 Airfoil
AIAA | 2005
|Grid sensivity study for the turbulent viscous flow around a NACA0015 airfoil at stall
British Library Conference Proceedings | 2005
|