Numerical and Experimental Wind Tunnel and Flight Testing of Active Flow Control for Modified NACA 643-618 Airfoil
53rd AIAA Aerospace Sciences Meeting
2015-01-01
Conference paper
Electronic Resource
English
Wind Tunnel and Free-Flight Testing of Active Flow Control for Modified NACA 61~3-618 Airfoil
British Library Conference Proceedings | 2013
|British Library Conference Proceedings | 2015
|Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap
Engineering Index Backfile | 1943
|Engineering Index Backfile | 1942
|