Airfoil Self Noise Reduction at Low Reynolds Numbers Using a Passive Flexible Trailing Edge
23rd AIAA/CEAS Aeroacoustics Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Experimental Research on Blunt Trailing-Edge Airfoil Sections at Low Reynolds Numbers
Online Contents | 1995
|Airfoil Trailing-edge Noise Reduction using Flow Suction
AIAA | 2018
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