Improving Accuracy of Airfoil Trailing Edge Noise Models with Turbulent Flow Anisotropy (2022)
Attributed to:
Effect of Separation and Stall on Aerofoil Noise
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.2514/6.2022-3105
Publication URI: http://dx.doi.org/10.2514/6.2022-3105
Type: Conference/Paper/Proceeding/Abstract