Numerical and Experimental Investigation of the Sound Generation in a Slat Cove of a High-Lift Wing Configuration
14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
2008-01-01
Conference paper
Electronic Resource
English
NUMERICAL INVESTIGATION OF HIGH-LIFT AIRFOIL FITTED WITH SLAT COVE FILLER
British Library Conference Proceedings | 2019
|Low noise wing slat system with rigid cove-filled slat
NTRS | 2013
|