Experimental Investigation of Turbulent Flow With Separation Over a NACA 4412 Airfoil at Angle of Attack 20 Degree
Fluids engineering conference ; 2002 ; Montreal, Canada
2002-01-01
P4
See also m03/14507-14510 for papers in print (4 vols.); Shelved in Conference Index. Held on CD-ROM
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
WAVEPACKETS IN TURBULENT FLOW OVER A NACA 4412 AIRFOIL
British Library Conference Proceedings | 2018
|Closed-Loop Feedback Control of the Turbulent Flow over a NACA-4412 Airfoil
British Library Conference Proceedings | 2005
|Plasma actuation effect on a NACA 4412 airfoil
Emerald Group Publishing | 2021
|POD Based Experimental Flow Control on a NACA-4412 Airfoil (Invited)
British Library Conference Proceedings | 2004
|