Airfoil Self Noise Reduction at Low Reynolds Numbers Using a Passive Flexible Trailing Edge
23rd AIAA/CEAS Aeroacoustics Conference
2017-01-01
Conference paper
Electronic Resource
English
Experimental Research on Blunt Trailing-Edge Airfoil Sections at Low Reynolds Numbers
Online Contents | 1995
|Experimental research on blunt trailing-edge airfoil sections at low Reynolds numbers
Tema Archive | 1995
|